WorldWideScience

Sample records for saab 9-5 aero

  1. Luzern saab uue kontserdimaja

    Index Scriptorium Estoniae

    1998-01-01

    Mais algavad Luzerni uue kontserdisaali akustiliste jm. näitajate testkontserdid. Uuest kontserdisaalist saab ka Luzerni kuulsate rahvusvaheliste festivalide pealava nii suvel kui lihavõtte aegu. Arhitekt Jean Nouvel, akustik Russell Johnson.

  2. Mis saab Potterist? / Jaanus Noormets

    Index Scriptorium Estoniae

    Noormets, Jaanus

    2007-01-01

    Eestis esilinastub 20. juulil Harry Potteri viies film "Harry Potter ja Fööniksi ordu" ("Harry Potter and the Order of the Phoenix"), režissöör David Yates : Ameerika Ühendriigid-Suurbritannia 2007. Alates 21. juulist saab raamatupoodidest osta seitsmendat ja ühtlasi viimast J. K. Rowlingu Potteri-sarja raamatut "Harry Potter and the Deathly Hallows"

  3. Eestist saab politseiriik / Roy Strider

    Index Scriptorium Estoniae

    Strider, Roy, 1974-

    2007-01-01

    Autori väitel ei ole politsei pärast kavandatavat avaliku koosoleku seaduse muutmist enam kohustatud inimestele teatama, kui nende eraelu puutumatust on jälitustoiminguga riivatud. Autori sõnul tähendab see, et Eestist saab politseiriik

  4. Kõik saab korda / Tamara Luuk

    Index Scriptorium Estoniae

    Luuk, Tamara, 1952-

    2010-01-01

    Rahvusvaheline videokunsti näitus "Kõik saab korda" Kumu Kunstimuuseumis 2. jaanuarini 2011. Kuraator Maria-Kristiina Soomre, kujundaja Berit Teeäär. Osalevad Marina Abramović (Serbia/USA), Eija-Liisa Ahtila (Soome), Kai Kaljo, Mike Marshall (Inglismaa), Ene-Liis Semper, Santeri Tuori (Soome), Guido van der Werve (Holland)

  5. 76 FR 31508 - Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 2000 Airplanes

    Science.gov (United States)

    2011-06-01

    ... pressure bulkhead, possibly resulting in in-flight decompression of the fuselage and injury to occupants...) originated by an aviation authority of another country to identify and correct an unsafe condition on an... pressure bulkhead of SAAB 2000 aeroplanes, located on the rear side of the bulkhead at the bottom outboard...

  6. Viru pataljon saab uue ülema

    Index Scriptorium Estoniae

    2006-01-01

    Ilmunud ka: Severnoje Poberezhje 22. juuli lk. 4. 31. juulist saab Viru üksik-jalaväepataljoni ülemaks major Urmet Reimann, senine ülem major Neeme Kaarna jätkab teenistust kirdekorpuse staabiohvitserina Poolas

  7. Esmalt saab raha Gildi fond / Piret Reiljan

    Index Scriptorium Estoniae

    Reiljan, Piret, 1983-

    2009-01-01

    Gild Arbitrage on Bulgaaria kinnisvaraprojektidesse investeerinud üle 100 miljoni krooni investorite ja võlausaldajate raha, kuid sealsete projektide realiseerimisel saab esimesena raha tagasi Gildi enda kinnisvarafond EEREIF

  8. Meltsiveski Konsumist saab korteritega supermarket / Nils Niitra

    Index Scriptorium Estoniae

    Niitra, Nils, 1975-

    2005-01-01

    Meltsiveski Konsumi kõrvale ehitatakse uus hoone, kus saab olema 30 korterit ja supermarket ning viimase katusel mängu- ja puhkeala. Juurdeehituse projekteeris arhitektuuribüroo Pluss arhitekt Indrek Allmann

  9. Admiral Cowan saab selga troopikavormid / Raul Vinni

    Index Scriptorium Estoniae

    Vinni, Raul

    2008-01-01

    Vahemerele suunduva miinijahtija "Admiral Cowan" meeskond saab esmakordselt Eestis valge troopikavormi. Miinijahtija osaleb NATO kiirreageerimisüksuse NRF-11 mereväekomponendis ja kuulub NATO miinitõrjeeskaadri SNMCMG1 koosseisu. 25. juulist kuni novembrini on miinijahtija Põhja regioonide miinitõrjeüksuse koosseisus

  10. Kui koolist saab villand / Aivi Pargi

    Index Scriptorium Estoniae

    Pargi, Aivi, 1950-

    2004-01-01

    Mitme riigi pedagoogid leiavad, et põhikoolieas kooli pooleli jätmine on uus sotsiaalne nähtus, mida saab ennetada õpetajatele uusi oskusi andes ning vanematega koostööd tehes. Kommenteerivad Riina Veidenbaum, Tiina Kivirand

  11. Mobiiliga saab hakata andma digitaalallkirja / Toivo Tänavsuu

    Index Scriptorium Estoniae

    Tänavsuu, Toivo

    2007-01-01

    EMT hakkab väljastama mobiiltelefoni SIM-kaarte, mis võimaldavad anda digitaalset allkirja. EMT lisateenuste ärijuhi Indrek Östermani selgitus. Lisad: Mobiiliga saab internetipanka minna ja digitaalallkirja anda; Keskkond muutub turvalisemaks

  12. Tehnikaromud saab peagi tasuta ära anda / Urmas Tooming

    Index Scriptorium Estoniae

    Tooming, Urmas

    2005-01-01

    13. augustist saab vana elektroonikat tasuta ära anda. MTÜ Eesti Elektroonikaromu on juba loonud selleks üle Eesti 44 kogumispunkti, EES-Ringlus ühingus endale konkurenti ei näe. Lisa: Vana tehnika

  13. Equipment for Aero-Optical Flow Imaging

    National Research Council Canada - National Science Library

    Catrakis, Haris

    2004-01-01

    The AFOSR/DURIP Grant has provided the funds to develop a new Aero-Optics Laboratory at UC Irvine, in order to do basic research on aero-optical laser beam propagation through high-speed turbulent flows...

  14. Evelin Ilves saab sama nimega firmalt tasuta uisutrikoosid / Kadri Jakobson

    Index Scriptorium Estoniae

    Jakobson, Kadri, 1970-

    2008-01-01

    Proua Evelin Ilves saab rulluisutrikood tootjafirmalt Ilves-Extra tasuta. Presidendi kantselei sõnul testib Rulluisuliidu president E. Ilves uisutrikood, mida Ilves-Extra alles kavatseb tootmisse võtta. Arvamust avaldavad Ilves-Extra juht Arvo Kivikas ja suhtekorraldusekspert Ivo Rull

  15. Piirivalve saab 147 miljoni eest uhke helikopteri / Sigrid Laev

    Index Scriptorium Estoniae

    Laev, Sigrid

    2005-01-01

    Eesti piirivalve saab helikopteri Agusta Bell, kopteri soetamine täidab Schnegen Facility programmi eesmärki, mille kohaselt tuleb EL-i välispiiride valve viia vastavusse Schengeni õigusruumi nõuetega. Raha ostmiseks annab abiprogramm Schengen Facility

  16. Taanlastest saab Türgi trump / Kaarel Tarand

    Index Scriptorium Estoniae

    Tarand, Kaarel, 1966-

    2006-01-01

    Türgi pakub end lääne ja islamimaailma peavahendajaks tsivilisatsioonide kokkupõrke ärahoidmiseks. Kui Türgi diplomaatial õnnestub pingeid leevendada, on Euroopal tema ees tänuvõlg, mida saab tasuda ainult EL-i liikmeks vastuvõtmisega, ütleb autor. Muhamedi karikatuuride avaldamise käsitlemisest Eestis

  17. 46 CFR 9.5 - Night, Sunday, and holiday defined.

    Science.gov (United States)

    2010-10-01

    ... 46 Shipping 1 2010-10-01 2010-10-01 false Night, Sunday, and holiday defined. 9.5 Section 9.5... COMPENSATION FOR OVERTIME SERVICES § 9.5 Night, Sunday, and holiday defined. (a) For the purpose of this part... term holiday shall mean only national legal public holidays, viz., January 1, February 22, May 30, July...

  18. 22 CFR 9.5 - Original classification authority.

    Science.gov (United States)

    2010-04-01

    ... 22 Foreign Relations 1 2010-04-01 2010-04-01 false Original classification authority. 9.5 Section 9.5 Foreign Relations DEPARTMENT OF STATE GENERAL SECURITY INFORMATION REGULATIONS § 9.5 Original classification authority. (a) Authority for original classification of information as Top Secret may be exercised...

  19. AeroMACS system characterization and demonstrations

    Science.gov (United States)

    Kerczewski, R. J.; Apaza, R. D.; Dimond, R. P.

    This The Aeronautical Mobile Airport Communications System (AeroMACS) is being developed to provide a new broadband wireless communications capability for safety critical communications in the airport surface domain, providing connectivity to aircraft and other ground vehicles as well as connections between other critical airport fixed assets. AeroMACS development has progressed from requirements definition through technology definition, prototype deployment and testing, and now into national and international standards development. The first prototype AeroMACS system has been deployed at the Cleveland Hopkins International Airport (CLE) and the adjacent NASA Glenn Research Center (GRC). During the past three years, extensive technical testing has taken place to characterize the performance of the AeroMACS prototype and provide technical support for the standards development process. The testing has characterized AeroMACS link and network performance over a variety of conditions for both fixed and mobile data transmission and has included basic system performance testing and fixed and mobile applications testing. This paper provides a summary of the AeroMACS performance testing and the status of standardization activities that the testing supports.

  20. EVPde aeg saab otsa / Uku Hänni

    Index Scriptorium Estoniae

    Hänni, Uku, 1943-

    2006-01-01

    Erastamisväärtpaberite kehtivusaeg saab käesoleva aastaga läbi. Sama ka Vooremaa 25. nov. 2006, lk. 4 ; Vooremaa : Palamuse Valla Teataja 25. nov. 2006, lk. 3 ; Kuulutaja 24. nov. 2006, lk. 4 ; Harjumaa 24. nov. 2006, lk. 2 ; Võrumaa Teataja 23. nov. 2006, lk. 2 ; Vali Uudised 29. nov. 2006, lk. 4 ; Vooremaa : Jõgeva Valla Teataja 2. Dets. 2006, lk. 3 ; Koit 2. Dets. 2006, lk. 6 ; Pärnu Postimees 7. Dets. 2006, lk. 15 ; Sakala 28. Dets. 2006, lk. 2

  1. Method of making an aero-derivative gas turbine engine

    Science.gov (United States)

    Wiebe, David J.

    2018-02-06

    A method of making an aero-derivative gas turbine engine (100) is provided. A combustor outer casing (68) is removed from an existing aero gas turbine engine (60). An annular combustor (84) is removed from the existing aero gas turbine engine. A first row of turbine vanes (38) is removed from the existing aero gas turbine engine. A can annular combustor assembly (122) is installed within the existing aero gas turbine engine. The can annular combustor assembly is configured to accelerate and orient combustion gasses directly onto a first row of turbine blades of the existing aero gas turbine engine. A can annular combustor assembly outer casing (108) is installed to produce the aero-derivative gas turbine engine (100). The can annular combustor assembly is installed within an axial span (85) of the existing aero gas turbine engine vacated by the annular combustor and the first row of turbine vanes.

  2. Aero-disaster in Port Harcourt, Nigeria: A case study

    African Journals Online (AJOL)

    Aero-disaster in Port Harcourt, Nigeria: A case study ... Aero-disaster in Nigeria is posing a serious problem to government, the public and relatives of victims, ..... which was recorded in one of our victim's relation, ... this communication.

  3. 75 FR 19673 - Petition for Exemption From the Vehicle Theft Prevention Standard; Saab

    Science.gov (United States)

    2010-04-15

    ... content requirements of Sec. 543.6. Saab stated that before the vehicle can operate, driver authentication... device will provide the five types of performance listed in Sec. 543.6(a)(3): promoting activation...

  4. Arnold Rüütel saab kõrgeima autasu / Silja Lättemäe

    Index Scriptorium Estoniae

    Lättemäe, Silja, 1952-

    2008-01-01

    President Arnold Rüütel saab president Toomas Hendrik Ilveselt Riigivapi ketiklassi teenetemärgi. Rahvaliit pole rahul, et A. Rüütel pole saanud ühtki riiklikku autasu oma panuse eest Eesti taasiseseisvumisse

  5. Ida-Virumaa keskkond saab 16,5 miljonit krooni / Külli Kriis

    Index Scriptorium Estoniae

    Kriis, Külli, 1961-

    2005-01-01

    Ilmunud ka: Severnoje Poberezhje 16. veebr. lk. 4. Keskkonnainvesteeringute keskuse (KIK) nõukogu otsustas keskkonnaprogrammi esimese vooru projektide rahastamise, mille järgi Ida-Virumaa saab üle 16 miljoni krooni. Tabel: Keskkonnaraha Ida-Virumaale

  6. Uudised : Konkursiedu. Laulva revolutsiooni meenutuseks. Vanemuise kontserdimaja saab juurdeehituse / Alo Põldmäe

    Index Scriptorium Estoniae

    Põldmäe, Alo, 1945-

    2001-01-01

    Eesti-taani duo saavutas 2.-4. juunini Prantsusmaal Poitiers's toimunud Euroopa Improvisatsiooniturniiril III koha. 20. juunil Teatri- ja Muusikamuuseumis toimuvast õhtust "Lauldes vabaks", kus meenutatakse Laulvat Revolutsiooni. Vanemuise kontserdimaja saab juurdeehituse

  7. E- Maksuametis saab tulusid deklareerida alates 15. veebruarist / Hannes Udde

    Index Scriptorium Estoniae

    Udde, Hannes

    2006-01-01

    Info 2005. aasta tulude (elektroonilise) deklareerimise kohta. Sama ka Võrumaa Teataja 28. jaan. 2006, lk. 6 ; Vooremaa 28. jaan. 2006, lk. 3, artiklis pealkiri kujul: Kuidas tuleb oma tulusid deklareerida ; Sõnumitooja 1. veeb. 2006, lk. 6 ; Meie Maa 1. veeb. 2006, lk. 4 ; Sakala 2. veeb. 2006, lk. 5, pealkiri kujul: Deklareerimine läheb lahti. ; Virumaa Teataja 2. veeb. 2006, lk. 9, pealkiri kujul: Maksumaksjad valmistuvad tulude deklareerimiseks. ; Vali Uudised 1. veeb. 2006, lk. 7 ; Valgamaalane 2. veeb. 2006, lk. 4, pealkiri kujul: E-maksuametis saab tulusid deklareerida ; Kuulutaja 3. veeb. 2006, lk. 11 ; Lääne Elu 7. veeb. 2006, lk. 2 ; Virumaa Nädalaleht 3. veeb. 2006, lk. 3 ; Hiiu Leht 10. veeb. 2006, lk. 5, pealkiri kujul: Maksumaksjad valmistuvad tulude deklareerimiseks ; Järva Teataja 16. veeb. 2006, lk. 2, pealkiri kujul: E-maksuamet alustas taas

  8. Surface modifications of aero-bearings

    International Nuclear Information System (INIS)

    Wang Yirong; Chen Jin; Nie Gao; Lu Haolin; Yang Qifa; Xu Qiu; Wang Peilu; Chen Yuanru; Liu Zhongyang

    1988-01-01

    Different ion beam techniques, i.e. ion beam mixing and ion implantation by either single or multi-element ions, were adopted to modify surface properties of aero-bearing samples that were made of GCr15 or Cr4Mo4V alloys, Results showed that corrosion behaviour and wear resistance of the samples treated with any of the techniques were improved significantly

  9. Common indoor and outdoor aero-allergens in South Africa

    African Journals Online (AJOL)

    Aero-allergens in South Africa that are also encountered around the world are listed in Table I. In addition to this wide range of common aero-allergens, South Africans are also exposed to a full range of food allergens, some of which, e.g. perlemoen (Haliotis midae) and other seafood allergens, are unique to this region.

  10. THE TREATMENT OF AERO-OTITIS MEDIA BY REDECOMPRESSION,

    Science.gov (United States)

    The precipitating event preceding the appearance of aero- otitis media is the development of a relative vacuum within the middle ear. The aim of...obtaining normal pressure relationships between the middle ear and the environment. In 27 of a group of 33 men with severe aero- otitis media , this

  11. Advanced technology for aero gas turbine components

    Energy Technology Data Exchange (ETDEWEB)

    1987-09-01

    The Symposium is aimed at highlighting the development of advanced components for new aero gas turbine propulsion systems in order to provide engineers and scientists with a forum to discuss recent progress in these technologies and to identify requirements for future research. Axial flow compressors, the operation of gas turbine engines in dust laden atmospheres, turbine engine design, blade cooling, unsteady gas flow through the stator and rotor of a turbomachine, gear systems for advanced turboprops, transonic blade design and the development of a plenum chamber burner system for an advanced VTOL engine are among the topics discussed.

  12. Aero and vibroacoustics of automotive turbochargers

    Energy Technology Data Exchange (ETDEWEB)

    Nguyen-Schaefer, Hung [Bosch Mahle Turbo Systems GmbH, Stuttgart (Germany)

    2013-02-01

    First book about the aeroacoustics of automotive turbochargers. Author of the book ''Rotordynamics of Automotive Turbochargers'', Springer, 2012. Written by an R and D expert in the turbocharger industry. Aero and Vibroacoustics of Automotive Turbochargers is a topic involving aspects from the working fields of thermodynamics of turbomachinery, aerodynamics, rotordynamics, and noise propagation computation. In this broadly interdisciplinary subject, thermodynamics of turbomachinery is used to design the turbocharger and to determine its operating conditions. Aerodynamics is needed to study the compressor flow dynamics and flow instabilities of rotating stall and surge, which can produce growling and whining-type noises. Rotordynamics is necessary to study rotor unbalance and self-excited oil-whirl instabilities, which lead to whistling and constant tone-type noises in rotating floating oil-film type bearings. For the special case of turbochargers using ball bearings, some high-order harmonic and wear noises also manifest in the rotor operating range. Lastly, noise propagation computation, based on Lighthill's analogy, is required to investigate airborne noises produced by turbochargers in passenger vehicles. The content of this book is intended for advanced undergraduates, graduates in mechanical engineering, research scientists and practicing engineers who want to better understand the interactions between these working fields and the resulting impact on the interesting topic of Aero and Vibroacoustics of Automotive Turbochargers.

  13. 32. keskkoolis saab jälle teatriharidust / Liisa-Indra Kärt

    Index Scriptorium Estoniae

    Kärt, Liisa-Indra

    2003-01-01

    Alates sügisest saab 32. keskkoolis jälle õppida teatrieriala, 29.03 toimunud vastuvõtukatsetel osales 50 teatrihuvilist noort. Konkurss treatriklassi oli ootamatult tihe, teatriklass tegutses 32. koolis alates selle loomisest aastal 1971-1980

  14. Ettevõtja saab raha ka otse Brüsselist / Silva Männik

    Index Scriptorium Estoniae

    Männik, Silva, 1974-

    2004-01-01

    Lisaks mitmetele Eesti asutustele, mis alates sellest aastast EL-i struktuurifondide kaudu raha jagama hakkavad, on ettevõtjatel võimalik taotleda erinevate programmide kaudu raha ka otse EL-i eelarvest. Lisa: Otse saab raha taotleda mitmest programmist

  15. Osa Pärnu poliitikuid saab ärimeestelt igakuist tasu / Teet Roosaar

    Index Scriptorium Estoniae

    Roosaar, Teet, 1963-

    2005-01-01

    Kuigi Pärnu uus linnavalitsus kärpis volikogu liikmete äriühingute nõukogudest makstavat tasu poole väiksemaks, saab osa poliitikuid endiselt lisasissetulekut, teiste seas linnakassast doteeritavalt Pärnu ATP-lt

  16. Aero-Assisted Pre-Stage for Ballistic and Aero-Assisted Launch Vehicles

    Science.gov (United States)

    Ustinov, Eugene A.

    2012-01-01

    A concept of an aero-assisted pre-stage is proposed, which enables launch of both ballistic and aero-assisted launch vehicles from conventional runways. The pre-stage can be implemented as a delta-wing with a suitable undercarriage, which is mated with the launch vehicle, so that their flight directions are coaligned. The ample wing area of the pre-stage combined with the thrust of the launch vehicle ensure prompt roll-out and take-off of the stack at airspeeds typical for a conventional jet airliner. The launch vehicle is separated from the pre-stage as soon as safe altitude is achieved, and the desired ascent trajectory is reached. Nominally, the pre-stage is non-powered. As an option, to save the propellant of the launch vehicle, the pre-stage may have its own short-burn propulsion system, whereas the propulsion system of the launch vehicle is activated at the separation point. A general non-dimensional analysis of performance of the pre-stage from roll-out to separation is carried out and applications to existing ballistic launch vehicle and hypothetical aero-assisted vehicles (spaceplanes) are considered.

  17. Aero and vibroacoustics of automotive turbochargers

    CERN Document Server

    Nguyen-Schäfer, Hung

    2013-01-01

    Aero and Vibroacoustics of Automotive Turbochargers is a topic involving aspects from the working fields of thermodynamics of turbomachinery, aerodynamics, rotordynamics, and noise propagation computation.   In this broadly interdisciplinary subject, thermodynamics of turbomachinery is used to design the turbocharger and to determine its operating conditions.  Aerodynamics is needed to study the compressor flow dynamics and flow instabilities of rotating stall and surge, which can produce growling and whining-type noises. Rotordynamics is necessary to study rotor unbalance and self-excited oil-whirl instabilities, which lead to whistling and constant tone-type noises in rotating floating oil-film type bearings. For the special case of turbochargers using ball bearings, some high-order harmonic and wear noises also manifest in the rotor operating range. Lastly, noise propagation computation, based on Lighthill’s analogy, is required to investigate airborne noises produced by turbochargers in passenger vehi...

  18. MEMS and mil/aero: technology push and market pull

    Science.gov (United States)

    Clifford, Thomas H.

    2001-04-01

    MEMS offers attractive solutions to high-density fluidics, inertial, optical, switching and other demanding military/aerospace (mil/aero) challenges. However, full acceptance must confront the realities of production-scale producibility, verifiability, testability, survivability, as well as long-term reliability. Data on these `..ilities' are crucial, and are central in funding and deployment decisions. Similarly, mil/aero users must highlight specific missions, environmental exposures, and procurement issues, as well as the quirks of its designers. These issues are particularly challenging in MEMS, because of the laws of physics and business economics, as well as the risks of deploying leading-edge technology into no-fail applications. This paper highlights mil/aero requirements, and suggests reliability/qualification protocols, to guide development effort and to reassure mil/aero users that MEMS labs are mindful of the necessary realities.

  19. Generic methods for aero-engine exhaust emission prediction

    NARCIS (Netherlands)

    Shakariyants, S.A.

    2008-01-01

    In the thesis, generic methods have been developed for aero-engine combustor performance, combustion chemistry, as well as airplane aerodynamics, airplane and engine performance. These methods specifically aim to support diverse emission prediction studies coupled with airplane and engine

  20. Aeronautical Mobile Airport Communications System (AeroMACS)

    Science.gov (United States)

    Budinger, James M.; Hall, Edward

    2011-01-01

    To help increase the capacity and efficiency of the nation s airports, a secure wideband wireless communications system is proposed for use on the airport surface. This paper provides an overview of the research and development process for the Aeronautical Mobile Airport Communications System (AeroMACS). AeroMACS is based on a specific commercial profile of the Institute of Electrical and Electronics Engineers (IEEE) 802.16 standard known as Wireless Worldwide Interoperability for Microwave Access or WiMAX (WiMax Forum). The paper includes background on the need for global interoperability in air/ground data communications, describes potential AeroMACS applications, addresses allocated frequency spectrum constraints, summarizes the international standardization process, and provides findings and recommendations from the world s first AeroMACS prototype implemented in Cleveland, Ohio, USA.

  1. Optics equations for aero-optical analysis

    Science.gov (United States)

    Sutton, George W.; Pond, John E.

    2011-05-01

    Aero-optical effects occur around moving air vehicles and impact passive imaging or active systems. The air flow around the vehicle is compressed, and often there is a turbulent shear and/or boundary layer both of which cause variations in the index of refraction. Examples of these are reconnaissance aircraft, the Stratospheric Observatory for Infrared Optics (SOFIA), and optically homing hypersonic interceptors. In other applications, a laser beam can be formed within the vehicle, and projected outward and focused on an object. These include the Airborne Laser Laboratory, Airborne Laser and the Airborne Tactical Laser. There are many compressible fluid mechanics computer programs that can predict the air density distribution of the surrounding flow field including density fluctuations in turbulent shear and/or boundary layers. It is necessary for the physical optics to be used to predict the properties of the ensuing image plane intensity distribution, whether passive or active. These include the time-averaged image blur circle and instantaneous realizations. (Ray tracing is a poor approximation that gives erroneous results for small aberrations.)

  2. Integrated Reconfigurable Aero and Propulsion Control for Improved Flight Safety of Commercial Aircraft, Phase I

    Data.gov (United States)

    National Aeronautics and Space Administration — The main objective of this project is to develop and test a novel innovative Integrated Reconfigurable Aero (i) Adaptive control design for the case of aero-only...

  3. Aero-Optic Evaluation Center (AOEC), Large Energy National Shock (LENS) Tunnels I & II

    Data.gov (United States)

    Federal Laboratory Consortium — The AOEC facility provides world class capability for aero-thermo-chemical, aerooptics and aero-propulsion testing in the Mach number range from 2.5 to 15 using the...

  4. Experimental Technique of Titanium Fire in Aero-engine

    Directory of Open Access Journals (Sweden)

    MI Guangbao

    2016-06-01

    Full Text Available Titanium fire is the typical catastrophic fault in the aero-engine. Aiming at the urgent demand for experimental technique of titanium fire from advanced high thrust-weight ratio aero-engine, the combustion technology and theory of titanium alloy based on friction oxygen concentration method (FOC were systematically studied. The evaluation method of fireproof property and the friction ignition model were built, and the fireproof mechanism was illustrated. By generalizing recent progress in experimental technique of titanium fire from three levels, including evolutionary rule, mechanism and prevention and control technology, the ideas and directions of experimental technique associated with the application research of titanium fire in the future were proposed, namely overall evaluation of fireproof property close to air flow environment of the aero-engine, prediction model of fireproof property and experimental verification of fireproof technique under the air flow environment of aero-engine. It is necessary to establish the prevention system of titanium fire in aero-engine, which contributes to the realization of "full titanium" in compressor and to the increase of high thrust-weight ratio.

  5. Vibration modelling and verifications for whole aero-engine

    Science.gov (United States)

    Chen, G.

    2015-08-01

    In this study, a new rotor-ball-bearing-casing coupling dynamic model for a practical aero-engine is established. In the coupling system, the rotor and casing systems are modelled using the finite element method, support systems are modelled as lumped parameter models, nonlinear factors of ball bearings and faults are included, and four types of supports and connection models are defined to model the complex rotor-support-casing coupling system of the aero-engine. A new numerical integral method that combines the Newmark-β method and the improved Newmark-β method (Zhai method) is used to obtain the system responses. Finally, the new model is verified in three ways: (1) modal experiment based on rotor-ball bearing rig, (2) modal experiment based on rotor-ball-bearing-casing rig, and (3) fault simulations for a certain type of missile turbofan aero-engine vibration. The results show that the proposed model can not only simulate the natural vibration characteristics of the whole aero-engine but also effectively perform nonlinear dynamic simulations of a whole aero-engine with faults.

  6. SIERRA/Aero User Manual Version 4.44

    Energy Technology Data Exchange (ETDEWEB)

    Sierra Thermal/Fluid Team

    2017-04-01

    SIERRA/Aero is a compressible fluid dynamics program intended to solve a wide variety compressible fluid flows including transonic and hypersonic problems. This document describes the commands for assembling a fluid model for analysis with this module, henceforth referred to simply as Aero for brevity. Aero is an application developed using the SIERRA Toolkit (STK). The intent of STK is to provide a set of tools for handling common tasks that programmers encounter when developing a code for numerical simulation. For example, components of STK provide field allocation and management, and parallel input/output of field and mesh data. These services also allow the development of coupled mechanics analysis software for a massively parallel computing environment. In the definitions of the commands that follow, the term Real_Max denotes the largest floating point value that can be represented on a given computer. Int_Max is the largest such integer value.

  7. SIERRA/Aero User Manual Version 4.46.

    Energy Technology Data Exchange (ETDEWEB)

    Sierra Thermal/Fluid Team

    2017-09-01

    SIERRA/Aero is a compressible fluid dynamics program intended to solve a wide variety compressible fluid flows including transonic and hypersonic problems. This document describes the commands for assembling a fluid model for analysis with this module, henceforth referred to simply as Aero for brevity. Aero is an application developed using the SIERRA Toolkit (STK). The intent of STK is to provide a set of tools for handling common tasks that programmers encounter when developing a code for numerical simulation. For example, components of STK provide field allocation and management, and parallel input/output of field and mesh data. These services also allow the development of coupled mechanics analysis software for a massively parallel computing environment. In the definitions of the commands that follow, the term Real_Max denotes the largest floating point value that can be represented on a given computer. Int_Max is the largest such integer value.

  8. SIERRA/Aero Theory Manual Version 4.44

    Energy Technology Data Exchange (ETDEWEB)

    Sierra Thermal/Fluid Team

    2017-04-01

    SIERRA/Aero is a two and three dimensional, node-centered, edge-based finite volume code that approximates the compressible Navier-Stokes equations on unstructured meshes. It is applicable to inviscid and high Reynolds number laminar and turbulent flows. Currently, two classes of turbulence models are provided: Reynolds Averaged Navier-Stokes (RANS) and hybrid methods such as Detached Eddy Simulation (DES). Large Eddy Simulation (LES) models are currently under development. The gas may be modeled either as ideal, or as a non-equilibrium, chemically reacting mixture of ideal gases. This document describes the mathematical models contained in the code, as well as certain implementation details. First, the governing equations are presented, followed by a description of the spatial discretization. Next, the time discretization is described, and finally the boundary conditions. Throughout the document, SIERRA/ Aero is referred to simply as Aero for brevity.

  9. SIERRA/Aero Theory Manual Version 4.46.

    Energy Technology Data Exchange (ETDEWEB)

    Sierra Thermal/Fluid Team

    2017-09-01

    SIERRA/Aero is a two and three dimensional, node-centered, edge-based finite volume code that approximates the compressible Navier-Stokes equations on unstructured meshes. It is applicable to inviscid and high Reynolds number laminar and turbulent flows. Currently, two classes of turbulence models are provided: Reynolds Averaged Navier-Stokes (RANS) and hybrid methods such as Detached Eddy Simulation (DES). Large Eddy Simulation (LES) models are currently under development. The gas may be modeled either as ideal, or as a non-equilibrium, chemically reacting mixture of ideal gases. This document describes the mathematical models contained in the code, as well as certain implementation details. First, the governing equations are presented, followed by a description of the spatial discretization. Next, the time discretization is described, and finally the boundary conditions. Throughout the document, SIERRA/ Aero is referred to simply as Aero for brevity.

  10. Vehicle Health Management Communications Requirements for AeroMACS

    Science.gov (United States)

    Kerczewski, Robert J.; Clements, Donna J.; Apaza, Rafael D.

    2012-01-01

    As the development of standards for the aeronautical mobile airport communications system (AeroMACS) progresses, the process of identifying and quantifying appropriate uses for the system is progressing. In addition to defining important elements of AeroMACS standards, indentifying the systems uses impacts AeroMACS bandwidth requirements. Although an initial 59 MHz spectrum allocation for AeroMACS was established in 2007, the allocation may be inadequate; studies have indicated that 100 MHz or more of spectrum may be required to support airport surface communications. Hence additional spectrum allocations have been proposed. Vehicle health management (VHM) systems, which can produce large volumes of vehicle health data, were not considered in the original bandwidth requirements analyses, and are therefore of interest in supporting proposals for additional AeroMACS spectrum. VHM systems are an emerging development in air vehicle safety, and preliminary estimates of the amount of data that will be produced and transmitted off an aircraft, both in flight and on the ground, have been prepared based on estimates of data produced by on-board vehicle health sensors and initial concepts of data processing approaches. This allowed an initial estimate of VHM data transmission requirements for the airport surface. More recently, vehicle-level systems designed to process and analyze VHM data and draw conclusions on the current state of vehicle health have been undergoing testing and evaluation. These systems make use of vehicle system data that is mostly different from VHM data considered previously for airport surface transmission, and produce processed system outputs that will be also need to be archived, thus generating additional data load for AeroMACS. This paper provides an analysis of airport surface data transmission requirements resulting from the vehicle level reasoning systems, within the context of overall VHM data requirements.

  11. Ständig förbättring på Saab Aerosystems

    OpenAIRE

    Johansson, Sandra

    2008-01-01

    The today’s high tech society with demands for new innovations and a cost effective work puts the companies to the test with many and complicated demands. To be a part of the evolution the companies have to establish good quality together with high profit. The global environment demands that companies work in line with total quality management and continuous improvements are a part of that. Saab has for a long time had one dominating product and one customer. The demands for continuous improv...

  12. Varssavi börs saab tänavu enam kui poolsada uustulnukat / Annika Matson

    Index Scriptorium Estoniae

    Matson, Annika, 1976-

    2005-01-01

    Ilmunud ka: Delovõje Vedomosti 16. märts lk. 29. Hollandi panga ING Securities Varssavi analüütik Piotr Palenik on kindel et sealsetesse börsifirmadesse voolab hetkel suurel hulgal välisinvestorite raha ning seetõttu on börsile tulemas rekordarv firmasid. Tabel: Suuremad Poola ettevõtted, mis tulevad tänavu börsile. Vt. samas: Välismaale investeerimise piirang; Eesti investor saab osta kõiki Varssavi börsi aktsiaid

  13. Uusi lasteaedu saab ehitada juba tänavu / Urve Palo

    Index Scriptorium Estoniae

    Palo, Urve, 1972-

    2008-01-01

    Ilmunud ka: Põhjarannik ja Severnoje Poberezhje 1. juuli lk. 2, Sõnumitooja ja Sakala 2. juuli lk. 2, Nädaline 3. juuli lk. 4, Meie Maa 7. juuli lk. 2, Vooremaa 10. juuli lk. 2. Linnade ja valdade lasteaedade ehitamiseks ja renoveerimiseks saavad toetust üle poole abi taotlejatest, riik saab eraldada nelja aasta jooksul 625 mln. krooni, lasteaedade investeerimisprogrammi kaudu rahastatakse 16 lasteaia ehitust ja 56 lasteaia renoveerimist, sel aastal luuakse riigi toetusel juurde üle 600 lasteaiakoha. Rahvastikuminister on veendunud, et riik peab programmi jätkama

  14. Overview of NASA Power Technologies for Space and Aero Applications

    Science.gov (United States)

    Beach, Raymond F.

    2014-01-01

    To achieve the ambitious goals that NASA has outlined for the next decades considerable development of power technology will be necessary. This presentation outlines the development objectives for both the space and aero applications. It further looks at the various power technologies that support these objectives and examines drivers that will be a driving force for future development.

  15. Assessment of Aero-radiometric Data of Southern Anambra Basin ...

    African Journals Online (AJOL)

    High-resolution aero-radiometric data from three radio-elements (Uranium, Potassium and Thorium) were used and processed independently to investigate the Southern Anambra basin for the prospect of producing radiogenic heat. The rock types in the study area were outlined while processing the elements in each rock ...

  16. Integrated evaluation of the geology, aero gamma spectrometry and aero magnetometry of the Sul-Riograndense Shield, southernmost Brazil

    Energy Technology Data Exchange (ETDEWEB)

    Hartmann, Leo A.; Savian, Jairo F., E-mail: leo.hartmann@ufrgs.br [Universidade Federal do Rio Grande do Sul (UFRS), Porto Alegre, RS (Brazil). Instituto de Geociencias; Lopes, William R. [Servico Geologico do Brasil (CPRM), Porto Alegre, RS (Brazil). Gerencia de Geologia e Mineracao

    2016-03-15

    An integrated evaluation of geology, aero gamma spectrometry and aero magnetometry of the Sul-Riograndense Shield is permitted by the advanced stage of understanding of the geology and geochronology of the southern Brazilian Shield and a 2010 airborne geophysical survey. Gamma rays are registered from the rocks near the surface and thus describe the distribution of major units in the shield, such as the Pelotas batholith, the juvenile São Gabriel terrane, the granulite-amphibolite facies Taquarembo terrane and the numerous granite intrusions in the foreland. Major structures are also observed, e.g., the Dorsal de Cangucu shear. Magnetic signals register near surface crustal compositions (analytic signal) and total crust composition (total magnetic signal), so their variation as measured indicates either shallow or whole crustal structures. The Cacapava shear is outstanding on the images as is the magnetic low along the N-S central portion of the shield. These integrated observations lead to the deepening of the understanding of the largest and even detailed structures of the Sul-Riograndense Shield, some to be correlated to field geology in future studies. Most significant is the presence of different provinces and their limits depending on the method used for data acquisition - geology, aero gamma spectrometry or aero magnetometry. (author)

  17. Rüütel saab poehinnast kolm korda odavama Audi / Küllike Rooväli

    Index Scriptorium Estoniae

    Rooväli, Küllike, 1969-

    2002-01-01

    Presidendi uueks ametiautoks saab Audi A8 4,2 Lang quattro. Audi tehas alandas presidendidele pakutava auto hinda ligi kolm korda. Pressinõunik Ester Šanki, Reval Auto juhi Aivar Toompere ja Silberauto pressiesindaja Üllar Borni kommentaarid

  18. Aero-Acoustic Modelling using Large Eddy Simulation

    International Nuclear Information System (INIS)

    Shen, W Z; Soerensen, J N

    2007-01-01

    The splitting technique for aero-acoustic computations is extended to simulate three-dimensional flow and acoustic waves from airfoils. The aero-acoustic model is coupled to a sub-grid-scale turbulence model for Large-Eddy Simulations. In the first test case, the model is applied to compute laminar flow past a NACA 0015 airfoil at a Reynolds number of 800, a Mach number of 0.2 and an angle of attack of 20 deg. The model is then applied to compute turbulent flow past a NACA 0015 airfoil at a Reynolds number of 100 000, a Mach number of 0.2 and an angle of attack of 20 deg. The predicted noise spectrum is compared to experimental data

  19. Sensor fault diagnosis of aero-engine based on divided flight status.

    Science.gov (United States)

    Zhao, Zhen; Zhang, Jun; Sun, Yigang; Liu, Zhexu

    2017-11-01

    Fault diagnosis and safety analysis of an aero-engine have attracted more and more attention in modern society, whose safety directly affects the flight safety of an aircraft. In this paper, the problem concerning sensor fault diagnosis is investigated for an aero-engine during the whole flight process. Considering that the aero-engine is always working in different status through the whole flight process, a flight status division-based sensor fault diagnosis method is presented to improve fault diagnosis precision for the aero-engine. First, aero-engine status is partitioned according to normal sensor data during the whole flight process through the clustering algorithm. Based on that, a diagnosis model is built for each status using the principal component analysis algorithm. Finally, the sensors are monitored using the built diagnosis models by identifying the aero-engine status. The simulation result illustrates the effectiveness of the proposed method.

  20. Sensor fault diagnosis of aero-engine based on divided flight status

    Science.gov (United States)

    Zhao, Zhen; Zhang, Jun; Sun, Yigang; Liu, Zhexu

    2017-11-01

    Fault diagnosis and safety analysis of an aero-engine have attracted more and more attention in modern society, whose safety directly affects the flight safety of an aircraft. In this paper, the problem concerning sensor fault diagnosis is investigated for an aero-engine during the whole flight process. Considering that the aero-engine is always working in different status through the whole flight process, a flight status division-based sensor fault diagnosis method is presented to improve fault diagnosis precision for the aero-engine. First, aero-engine status is partitioned according to normal sensor data during the whole flight process through the clustering algorithm. Based on that, a diagnosis model is built for each status using the principal component analysis algorithm. Finally, the sensors are monitored using the built diagnosis models by identifying the aero-engine status. The simulation result illustrates the effectiveness of the proposed method.

  1. 76 FR 77108 - Airworthiness Directives; International Aero Engines Turbofan Engines

    Science.gov (United States)

    2011-12-12

    ... Airworthiness Directives; International Aero Engines Turbofan Engines AGENCY: Federal Aviation Administration...-D5, V2530-A5, and V2533-A5 turbofan engines. This AD was prompted by three reports of high- pressure..., V2524-A5, V2525-D5, V2527-A5, V2527E-A5, V2527M-A5, V2528- D5, V2530-A5, and V2533-A5 turbofan engines...

  2. Maintenance Decision Based on Data Fusion of Aero Engines

    Directory of Open Access Journals (Sweden)

    Huawei Wang

    2013-01-01

    Full Text Available Maintenance has gained a great importance as a support function for ensuring aero engine reliability and availability. Cost-effectiveness and risk control are two basic criteria for accurate maintenance. Given that aero engines have much condition monitoring data, this paper presents a new condition-based maintenance decision system that employs data fusion for improving accuracy of reliability evaluation. Bayesian linear model has been applied, so that the performance degradation evaluation of aero engines could be realized. A reliability evaluation model has been presented based on gamma process, which achieves the accurate evaluation by information fusion. In reliability evaluation model, the shape parameter is estimated by the performance degradation evaluation result, and the scale parameter is estimated by failure, inspection, and repair information. What is more, with such reliability evaluation as input variables and by using particle swarm optimization (PSO, a stochastic optimization of maintenance decision for aircraft engines has been presented, in which the effectiveness and the accuracy are demonstrated by a numerical example.

  3. Real-world adjustments of driver seat and head restraint in Saab 9-3 vehicles.

    Science.gov (United States)

    Carlsson, Anna; Pipkorn, Linda; Kullgren, Anders; Svensson, Mats

    2017-05-19

    Whiplash-associated disorder (WAD), commonly denoted whiplash injury, is a worldwide problem. These injuries occur at relatively low changes of velocity (typically whiplash injury than males.  Improved seat design is the prevailing means of increasing the protection of whiplash injury for occupants in rear impacts. Since 1997, more advanced whiplash protection systems have been introduced on the market, the Saab Active Head Restraint (SAHR) being one of the most prominent. The SAHR-which is height adjustable-is mounted to a pressure plate in the seatback by means of a spring-resisted link mechanism.  Nevertheless, studies have shown that seats equipped with reactive head restraints (such as the SAHR) have a very high injury-reducing effect for males (∼60-70%) but very low or no reduction effect for females. One influencing factor could be the position of the head restraint relative to the head, because a number of studies have reported that adjustable head restraints often are incorrectly positioned by drivers.  The aim was to investigate how female and male Saab drivers adjust the seat in the car they drive the most. The seated positions of drivers in stationary conditions have been investigated in a total of 76 volunteers (34 females, 42 males) who participated in the study. Inclusion criteria incorporated driving a Saab 9-3 on a regularly basis. The majority of the volunteers (89%) adjusted the head restraint to any of the 3 uppermost positions and as many as 59% in the top position.  The average vertical distance between the top of the head and the top of the head restraint (offset) increase linearly with increasing statures, from an average of -26 mm (head below the head restraint) for small females to an average of 82 mm (head above the head restraint) for large males. On average, the offset was 23 mm for females, which is within a satisfactory range and in accordance with recommendations; the corresponding value for males was 72 mm.

  4. Eesti vetesse trügiv Gazprom saab suure relvastatud üksuse / Lauri Linnamäe

    Index Scriptorium Estoniae

    Linnamäe, Lauri

    2007-01-01

    Ilmunud ka: Postimees : na russkom jazõke, 17. apr. 2007, lk. 5. Vene gaasimonopol Gazprom saab Vene riigilt ilmselt volitused Läänemerre plaanitava gaasijuhtme kaitsmiseks tuhandeist võitlejaist koosneva hästirelvastatud eraarmee loomiseks, riigiduumas algatatud vastavast seaduseelnõust. Parlamendiliikmete Igor Gräzini ja Marko Mihkelsoni arvamused sõjalis-poliitilistest ohtudest. Skeem: Gazprom võib tuua eraarmee Vene-Saksa gaasijuhet kaitsma

  5. 78 FR 22168 - Airworthiness Directives; International Aero Engines AG Turbofan Engines

    Science.gov (United States)

    2013-04-15

    ... Airworthiness Directives; International Aero Engines AG Turbofan Engines AGENCY: Federal Aviation Administration... International Aero Engines AG (IAE), V2525-D5 and V2528-D5 turbofan engines, with a certain No. 4 bearing... turbofan engines, serial numbers V20001 through V20285, with No. 4 bearing internal scavenge tube, part...

  6. 76 FR 60396 - Airworthiness Directives; Piaggio Aero Industries S.p.A. Airplanes

    Science.gov (United States)

    2011-09-29

    ...., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service... on other P.180 aeroplanes, and Piaggio Aero Industries (PAI) had issued Service Bulletin (SB) No. 80... information by examining the MCAI in the AD docket. Relevant Service Information Piaggio Aero Industries S.p.A...

  7. 77 FR 35888 - Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Airplanes

    Science.gov (United States)

    2012-06-15

    ...., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service.... Relevant Service Information PIAGGIO AERO INDUSTRIES S.p.A. has issued Service Bulletin No. 80- 0318, dated... Instructions of Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80-0318, revision 2, dated March...

  8. 78 FR 36691 - Airworthiness Directives; Piaggio Aero Industries S.p.A Airplanes

    Science.gov (United States)

    2013-06-19

    ...., Washington, DC 20590, between 9 a.m. and 5 p.m., Monday through Friday, except Federal holidays. For service... condition, Piaggio Aero Industries (PAI) issued Service Bulletin (SB) 80-0345 to provide instructions for... in the AD docket. Relevant Service Information Piaggio Aero Industries S.p.A. has issued Mandatory...

  9. 76 FR 27872 - Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model P-180 Airplanes

    Science.gov (United States)

    2011-05-13

    ... through Friday, except Federal holidays. For service information identified in this AD, contact Piaggio... accomplishment instructions of Piaggio Aero Industries Alert Service Bulletin ASB- 80-0324, step 5, this AD.... Relevant Service Information PIAGGIO AERO INDUSTRIES S.p.A has issued Service Bulletin (Mandatory) N.: 80...

  10. 78 FR 69600 - Airworthiness Directives; Piaggio Aero Industries S.p.A Airplanes

    Science.gov (United States)

    2013-11-20

    ... p.m., Monday through Friday, except Federal holidays. For service information identified in this.... To address this potential unsafe condition, Piaggio Aero Industries (PAI) issued Service [[Page 69601... Service Information Piaggio Aero Industries S.p.A. has issued Mandatory Service Bulletin No.: 80-0381, Rev...

  11. 76 FR 54403 - Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

    Science.gov (United States)

    2011-09-01

    ... Federal holidays. For service information identified in this proposed AD, contact Piaggio Aero Industries... Service Information Piaggio Aero Industries S.p.A. has issued Mandatory Service Bulletin No. 80-0304... Accomplishment Instructions of Piaggio Aero Industries S.p.A. Mandatory Service Bulletin No. 80-0304, dated July...

  12. Aero-acoustics noise assessment for Wind-Lens turbine

    International Nuclear Information System (INIS)

    Hashem, I.; Mohamed, M.H.; Hafiz, A.A.

    2017-01-01

    This paper introduces an aero-acoustic computational study that investigates the noise caused by one of the most promising wind energy conversion concepts, namely the 'Wind-Lens' technology. The hybrid method - where the flow field and acoustic field are solved separately, was deemed to be an appropriate tool to compute this study. The need to investigate this phenomenon increased gradually, since the feasibility of utilizing Wind-Lens turbine within densely populated cities and urban areas depends largely on their noise generation. Ffowcs Williams-Hawkings (FW-H) equation and its integral solution are used to predict the noise radiating to the farfield. CFD Simulations of transient three-dimensional flow field using (URANS) unsteady Reynolds-averaged Navier-Stokes equations are computed to acquire the acoustic sources location and sound intensity. Then, the noise propagates from the before-mentioned sources to pre-defined virtual microphones positioned in different locations. ANSYS-FLUENT is used to calculate the flow field on and around such turbines which is required for the FW-H code. Some effective parameters are investigated such as Wind-Lens shape, brim height and tip speed ratio. Comparison of the noise emitted from the bare wind turbine and different types of Wind-Lens turbine reveals that, the Wind-Lens generates higher noise intensity. - Highlights: • Aero-acoustic noise generated by wind turbines are one of the major challenges. • Noise from wind turbine equipped with a brimmed diffuser is investigated. • A computational aero-acoustic study using the hybrid method is introduced. • Effective parameters are studied such Wind-Lens shape, brim height and speed ratio. • The optimal shape has a moderate power coefficient and the less noise generation.

  13. Future NASA Power Technologies for Space and Aero Propulsion Applications

    Science.gov (United States)

    Soeder, James F.

    2015-01-01

    To achieve the ambitious goals that NASA has outlined for the next decades considerable development of power technology will be necessary. This presentation outlines the development objectives for both space and aero applications. It further looks at the various power technologies that support these objectives and examines drivers that will be a driving force for future development. Finally, the presentation examines what type of non-traditional learning areas should be emphasized in student curriculum so that the engineering needs of the third decade of the 21st Century are met.

  14. Aero-acoustic noise of wind turbines. Noise prediction models

    Energy Technology Data Exchange (ETDEWEB)

    Maribo Pedersen, B. [ed.

    1997-12-31

    Semi-empirical and CAA (Computational AeroAcoustics) noise prediction techniques are the subject of this expert meeting. The meeting presents and discusses models and methods. The meeting may provide answers to the following questions: What Noise sources are the most important? How are the sources best modeled? What needs to be done to do better predictions? Does it boil down to correct prediction of the unsteady aerodynamics around the rotor? Or is the difficult part to convert the aerodynamics into acoustics? (LN)

  15. Optimization of Aero Engine Acceleration Control in Combat State Based on Genetic Algorithms

    Science.gov (United States)

    Li, Jie; Fan, Ding; Sreeram, Victor

    2012-03-01

    In order to drastically exploit the potential of the aero engine and improve acceleration performance in the combat state, an on-line optimized controller based on genetic algorithms is designed for an aero engine. For testing the validity of the presented control method, detailed joint simulation tests of the designed controller and the aero engine model are performed in the whole flight envelope. Simulation test results show that the presented control algorithm has characteristics of rapid convergence speed, high efficiency and can fully exploit the acceleration performance potential of the aero engine. Compared with the former controller, the designed on-line optimized controller (DOOC) can improve the security of the acceleration process and greatly enhance the aero engine thrust in the whole range of the flight envelope, the thrust increases an average of 8.1% in the randomly selected working states. The plane which adopts DOOC can acquire better fighting advantage in the combat state.

  16. Computation and analysis of backward ray-tracing in aero-optics flow fields.

    Science.gov (United States)

    Xu, Liang; Xue, Deting; Lv, Xiaoyi

    2018-01-08

    A backward ray-tracing method is proposed for aero-optics simulation. Different from forward tracing, the backward tracing direction is from the internal sensor to the distant target. Along this direction, the tracing in turn goes through the internal gas region, the aero-optics flow field, and the freestream. The coordinate value, the density, and the refractive index are calculated at each tracing step. A stopping criterion is developed to ensure the tracing stops at the outer edge of the aero-optics flow field. As a demonstration, the analysis is carried out for a typical blunt nosed vehicle. The backward tracing method and stopping criterion greatly simplify the ray-tracing computations in the aero-optics flow field, and they can be extended to our active laser illumination aero-optics study because of the reciprocity principle.

  17. Interference Analysis Status and Plans for Aeronautical Mobile Airport Communications System (AeroMACS)

    Science.gov (United States)

    Kerczewski, Robert J.; Wilson, Jeffrey D.

    2010-01-01

    Interference issues related to the operation of an aeronautical mobile airport communications system (AeroMACS) in the C-Band (specifically 5091-5150 MHz) is being investigated. The issue of primary interest is co-channel interference from AeroMACS into mobile-satellite system (MSS) feeder uplinks. The effort is focusing on establishing practical limits on AeroMACS transmissions from airports so that the threshold of interference into MSS is not exceeded. The analyses are being performed with the software package Visualyse Professional, developed by Transfinite Systems Limited. Results with omni-directional antennas and plans to extend the models to represent AeroMACS more accurately will be presented. These models should enable realistic analyses of emerging AeroMACS designs to be developed from NASA Test Bed, RTCA 223, and European results.

  18. Optimization of Heat Exchangers for Intercooled Recuperated Aero Engines

    Directory of Open Access Journals (Sweden)

    Dimitrios Misirlis

    2017-03-01

    Full Text Available In the framework of the European research project LEMCOTEC, a section was devoted to the further optimization of the recuperation system of the Intercooled Recuperated Aero engine (IRA engine concept, of MTU Aero Engines AG. This concept is based on an advanced thermodynamic cycle combining both intercooling and recuperation. The present work is focused only on the recuperation process. This is carried out through a system of heat exchangers mounted inside the hot-gas exhaust nozzle, providing fuel economy and reduced pollutant emissions. The optimization of the recuperation system was performed using computational fluid dynamics (CFD computations, experimental measurements and thermodynamic cycle analysis for a wide range of engine operating conditions. A customized numerical tool was developed based on an advanced porosity model approach. The heat exchangers were modeled as porous media of predefined heat transfer and pressure loss behaviour and could also incorporate major and critical heat exchanger design decisions in the CFD computations. The optimization resulted in two completely new innovative heat exchanger concepts, named as CORN (COnical Recuperative Nozzle and STARTREC (STraight AnnulaR Thermal RECuperator, which provided significant benefits in terms of fuel consumption, pollutants emission and weight reduction compared to more conventional heat exchanger designs, thus proving that further optimization potential for this technology exists.

  19. AeroVironment technician checks a Helios solar cell panel

    Science.gov (United States)

    2000-01-01

    A technician at AeroVironment's Design Development Center in Simi Valley, California, checks a panel of silicon solar cells for conductivity and voltage. The bi-facial cells, fabricated by SunPower, Inc., of Sunnyvale, California, are among 64,000 solar cells which have been installed on the Helios Prototype solar-powered aircraft to provide power to its 14 electric motors and operating systems. Developed by AeroVironment under NASA's Environmental Research Aircraft and Sensor Technology (ERAST) project, the Helios Prototype is the forerunner of a planned fleet of slow-flying, long duration, high-altitude aircraft which can perform atmospheric science missions and serve as telecommunications relay platforms in the stratosphere. Target goals set by NASA for the giant 246-foot span flying wing include reaching and sustaining subsonic horizontal flight at 100,000 feet altitude in 2001, and sustained continuous flight for at least four days and nights above 50,000 feet altitude with the aid of a regenerative fuel cell-based energy storage system now under development in 2003.

  20. Spectral Behavior of Weakly Compressible Aero-Optical Distortions

    Science.gov (United States)

    Mathews, Edwin; Wang, Kan; Wang, Meng; Jumper, Eric

    2016-11-01

    In classical theories of optical distortions by atmospheric turbulence, an appropriate and key assumption is that index-of-refraction variations are dominated by fluctuations in temperature and the effects of turbulent pressure fluctuations are negligible. This assumption is, however, not generally valid for aero-optical distortions caused by turbulent flow over an optical aperture, where both temperature and pressures fluctuations may contribute significantly to the index-of-refraction fluctuations. A general expression for weak fluctuations in refractive index is derived using the ideal gas law and Gladstone-Dale relation and applied to describe the spectral behavior of aero-optical distortions. Large-eddy simulations of weakly compressible, temporally evolving shear layers are then used to verify the theoretical results. Computational results support theoretical findings and confirm that if the log slope of the 1-D density spectrum in the inertial range is -mρ , the optical phase distortion spectral slope is given by - (mρ + 1) . The value of mρ is then shown to be dependent on the ratio of shear-layer free-stream densities and bounded by the spectral slopes of temperature and pressure fluctuations. Supported by HEL-JTO through AFOSR Grant FA9550-13-1-0001 and Blue Waters Graduate Fellowship Program.

  1. Association of promoter methylation of VGF and PGP9.5 with ovarian cancer progression.

    Directory of Open Access Journals (Sweden)

    Mariana Brait

    Full Text Available To elucidate the role of biological and clinical impact of aberrant promoter hypermethylation (PH in ovarian cancer (OC.PH of PGP9.5, HIC1, AIM1, APC, PAK3, MGMT, KIF1A, CCNA1, ESR1, SSBP2, GSTP1, FKBP4 and VGF were assessed by quantitative methylation specific PCR (QMSP in a training set. We selected two genes (VGF and PGP9.5 for further QMSP analysis in a larger independent validation (IV set with available clinical data. Biologic relevance of VGF gene was also evaluated.PH frequency for PGP9.5 and VGF were 85% (316/372 and 43% (158/366 respectively in the IV set of samples while no PH was observed in controls. In 372 OC cases with available follow up, PGP9.5 and VGF PH were correlated with better patient survival [Hazard Ratios (HR for overall survival (OS were 0.59 (95% Confidence Intervals (CI  = 0.42-0.84, p = 0.004, and 0.73 (95%CI = 0.55-0.97, p = 0.028 respectively, and for disease specific survival (DSS were 0.57 (95%CI 0.39-0.82, p = 0.003 and 0.72 (95%CI 0.54-0.96, p = 0.027. In multivariate analysis, VGF PH remained an independent prognostic factor for OS (HR 0.61, 95%CI 0.43-0.86, p<0.005 and DSS (HR 0.58, 95%CI 0.41-0.83, p<0.003. Furthermore, PGP9.5 PH was significantly correlated with lower grade, early stage tumors, and with absence of residual disease. Forced expression of VGF in OC cell lines inhibited cell growth.Our results indicate that VGF and PGP9.5 PH are potential biomarkers for ovarian carcinoma. Confirmatory cohorts with longitudinal follow-up are required in future studies to define the clinical impact of VGF and PGP9.5 PH before clinical application.

  2. Predicting Cavitation on Marine and Hydrokinetic Turbine Blades with AeroDyn V15.04

    Energy Technology Data Exchange (ETDEWEB)

    Murray, Robynne [National Renewable Energy Laboratory (NREL), Golden, CO (United States)

    2017-09-14

    Cavitation is an important consideration in the design of marine and hydrokinetic (MHK) turbines. The National Renewable Energy Laboratory's AeroDyn performance code was originally developed for horizontal-axis wind turbines and did not have the capability to predict cavitation inception. Therefore, AeroDyn has been updated to include the ability to predict cavitation on MHK turbines based on user-specified vapor pressure and submerged depth. This report outlines a verification of the AeroDyn V15.04 performance code for MHK turbines through a comparison to publicly available performance data.

  3. Cancer chemotherapy of the upper aero digestive tract

    International Nuclear Information System (INIS)

    Vedrine, L.; Chargari, C.; Le Moulec, S.; Fayolle, M.; Ceccaldi, B.; Bauduceau, O.

    2008-01-01

    Tumours of the upper aero digestive tract represent the sixth most frequent kind of cancer in France and throughout the world. If the localised forms may be controlled in the long run in two thirds of cases by surgery or radiotherapy, only one third of locally advanced forms are accessible to a cure after association from radiotherapy and chemotherapy. Besides, with a median of survival less than six months, metastatic tumours present a catastrophic spontaneous prognosis among patients with a medical ground that is often heavily deteriorated by prolonged exposure to alcohol and tobacco. Thus, there is a necessity to implement adapted therapeutic strategies to each patient and based on satisfactory proof levels of effectiveness. Optimisation of existing chemotherapy protocols and development of new therapies, in particular of targeted therapies, remain an important objective in the hope to improve results of treatments in locally advanced and metastatic cancers of the oral cavity. (authors)

  4. Fungal Competitors Affect Production of Antimicrobial Lipopeptides in Bacillus subtilis Strain B9-5.

    Science.gov (United States)

    DeFilippi, Stefanie; Groulx, Emma; Megalla, Merna; Mohamed, Rowida; Avis, Tyler J

    2018-04-01

    Bacillus subtilis has shown success in antagonizing plant pathogens where strains of the bacterium produce antimicrobial cyclic lipopeptides (CLPs) in response to microbial competitors in their ecological niche. To gain insight into the inhibitory role of these CLPs, B. subtilis strain B9-5 was co-cultured with three pathogenic fungi. Inhibition of mycelial growth and spore germination was assessed and CLPs produced by B. subtilis B9-5 were quantified over the entire period of microbial interaction. B. subtilis B9-5 significantly inhibited mycelial growth and spore germination of Fusarium sambucinum and Verticillium dahliae, but not Rhizopus stolonifer. LC-MS analysis revealed that B. subtilis differentially produced fengycin and surfactin homologs depending on the competitor. CLP quantification suggested that the presence of Verticillium dahliae, a fungus highly sensitive to the compounds, caused an increase followed by a decrease in CLP production by the bacterium. In co-cultures with Fusarium sambucinum, a moderately sensitive fungus, CLP production increased more gradually, possibly because of its slower rate of spore germination. With co-cultures of the tolerant fungus Rhizopus stolonifer, B. subtilis produced high amounts of CLPs (per bacterial cell) for the duration of the interaction. Variations in CLP production could be explained, in part, by the pathogens' overall sensitivities to the bacterial lipopeptides and/or the relative growth rates between the plant pathogen and B. subtilis. CLP production varied substantially temporally depending on the targeted fungus, which provides valuable insight concerning the effectiveness of B. subtilis B9-5 protecting its ecological niche against the ingress of these pathogens.

  5. Marketingový mix volejbalového klubu Aero Odolena Voda

    OpenAIRE

    Hons, Michal

    2013-01-01

    Title: Volleyball club Aero Odolena Voda marketing mix analysis Targets: To perform an overall evaluation of the current Aero Odolena Voda marketing mix, using SWOT analysis bring strenghts and weaknesses to light. Based on this analysis suggest possible modification that would lead to a better marketing mix. Methods: Using qualitative methods such as interview, alongside with quantitative methods such as questioning, SWOT analysis and using secundary dates. Results: The specific modification...

  6. A SERIES OF UNCOMMON FOREIGN BODIES PRESENTING IN THE AERO-DIGESTIVE TRACT

    Directory of Open Access Journals (Sweden)

    Jitendra Singh

    2016-02-01

    Full Text Available Foreign body impacted in the aero-digestive tract is one of the earliest reported problems. Coins, buttons, marbles, crayons, parts of toys etc. are the most commonly ingested foreign bodies in children. Fish, meat and chicken bones, dentures, nails etc.the most common foreign bodies ingested by adultsWe report a series of unusual foreign body ingestion in aero-digestive tract and their management by endoscopic retrieval.

  7. The DAN-AERO MW experiments. Final report

    Energy Technology Data Exchange (ETDEWEB)

    Aagaard Madsen, H.; Bak, C.; Schmidt Paulsen, U.; Gaunaa, M. (Risoe DTU, Roskilde (Denmark)); Fuglsang, P. (LM Glasfiber, Kolding (Denmark)); Romblad, J.; Olesen, N.A. (Vestas Wind Systems, Ringkoebing (Denmark)); Enevoldsen, P.; Laursen, J. (Siemens Wind Power, Ballerup (Denmark)); Jensen, Leo (DONG Energy, Fredericia (Denmark))

    2010-09-15

    This report describes the DAN-AERO MW experiments carried out within a collaborative, three years research project between Risoe DTU and the industrial partners LM Glasfiber, Siemens Wind Power, Vestas Wind Systems A/S and the utility company DONG Energy. The main objective of the project was to establish an experimental data base which can provide new insight into a number of fundamental aerodynamic and aero-acoustic issues, important for the design and operation of MW size turbines. The most important issue is the difference between airfoil characteristics measured under 2D, steady conditions in a wind tunnel and the unsteady 3D flow conditions on a rotor. The different transition characteristics might explain some of the differences between the 2D and 3D airfoil data and the experiments have been set up to provide data on this subject. The overall experimental approach has been to carry out a number of coordinated, innovative measurements on full scale MW size rotors as well as on airfoils for MW size turbines in wind tunnels. Shear and turbulence inflow characteristics were measured on a Siemens 3.6 MW turbine with a five hole pitot tube. Pressure and turbulent inflow characteristics were measured on a 2MW NM80 turbine with an 80 m rotor. One of the LM38.8 m blades on the rotor was replaced with a new LM38.8 m blade where instruments for surface pressure measurements at four radial sections were build into the blade during the blade production process. Additionally, the outmost section on the blade was further instrumented with around 50 microphones for high frequency surface pressure measurements. The surface pressure measurements have been correlated with inflow measurements from four five hole pitot tubes and two sensors for measuring the high frequency (50 Hz to10 kHz) contents of the inflow turbulence. In parallel, 2D wind tunnel measurements on common airfoils for wind turbine applications have been conducted in three different wind tunnels at Delft

  8. Experimental investigation on aero-optics of supersonic turbulent boundary layers.

    Science.gov (United States)

    Ding, Haolin; Yi, Shihe; Zhu, Yangzhu; He, Lin

    2017-09-20

    Nanoparticle-based planar laser scattering was used to measure the density distribution of the supersonic (Ma=3.0) turbulent boundary layer and the optical path difference (OPD), which is quite crucial for aero-optics study. Results were obtained using ray tracing. The influences of different layers in the boundary layer, turbulence scales, and light incident angle on aero-optics were examined, and the underlying flow physics were analyzed. The inner layer plays a dominant role, followed by the outer layer. One hundred OPD rms of the outer layer at different times satisfy the normal distribution better than that of the inner layer. Aero-optics induced by the outer layer is sensitive to the filter scale. When induced by the inner layer, it is not sensitive to the filter scale. The vortices with scales less than the Kolmogorov scale (=46.0  μm) have little influence on the aero-optics and could be ignored; the validity of the smallest optically active scale (=88.1  μm) proposed by Mani is verified, and vortices with scales less than that are ignored, resulting in a 1.62% decay of aero-optics; the filter with a width of 16-grid spacing (=182.4  μm) decreases OPD rms by 7.04%. With the increase of the angle between the wall-normal direction and the light-incident direction, the aero-optics becomes more serious, and the difference between the distribution of the OPD rms and the normal distribution increases. The difficulty of aero-optics correction is increased. Light tilted toward downstream experiences more distortions than when tilted toward upstream at the same angle relative to the wall-normal direction.

  9. Aero-methods and engineering research and development

    Energy Technology Data Exchange (ETDEWEB)

    Peterson, R K

    1979-01-01

    There is presently a sharp, ongoing increase in the volume of work being conducted throughout the country associated with the development of natural gas fields as well as the resulting accelerated development of major gas trunklines. Aero-methods have presently found wide application in the engineering and planning of equipment for such projects. Success has been obtained by the increased quantity and quality of the available engineering information: The ''Giprospetsgaz'' Institute is using aerial photography as the basis for selecting pipeline routes and to more accurately determine the equipment requirements along proposed trunklines such as for compressors, gas transfer stations, electrical power substations, worker settlements, water and transport infrastructure and communications. These requirements are the most important factors in reducing capital operating expenditures. The greatest savings, in economic terms, can be achieved by avoiding sparsely settled or uninhabited areas as much as possible. Similiarly, aerial photography coupled with computer application aids in the solution of engineering problems. Third-generation computers are recommended for this process.

  10. MiR-9-5p promotes MSC migration by activating β-catenin signaling pathway.

    Science.gov (United States)

    Li, Xianyang; He, Lihong; Yue, Qing; Lu, Junhou; Kang, Naixin; Xu, Xiaojing; Wang, Huihui; Zhang, Huanxiang

    2017-07-01

    Mesenchymal stem cells (MSCs) have the potential to treat various tissue damages, but the very limited number of cells that migrate to the damaged region strongly restricts their therapeutic applications. Full understanding of mechanisms regulating MSC migration will help to improve their migration ability and therapeutic effects. Increasing evidence shows that microRNAs play important roles in the regulation of MSC migration. In the present study, we reported that miR-9-5p was upregulated in hepatocyte growth factor -treated MSCs and in MSCs with high migration ability. Overexpression of miR-9-5p promoted MSC migration, whereas inhibition of endogenous miR-9-5p decreased MSC migration. To elucidate the underlying mechanism, we screened the target genes of miR-9-5p and report for the first time that CK1α and GSK3β, two inhibitors of β-catenin signaling pathway, were direct targets of miR-9-5p in MSCs and that overexpression of miR-9-5p upregulated β-catenin signaling pathway. In line with these data, inhibition of β-catenin signaling pathway by FH535 decreased the miR-9-5p-promoted migration of MSCs, while activation of β-catenin signaling pathway by LiCl rescued the impaired migration of MSCs triggered by miR-9-5p inhibitor. Furthermore, the formation and distribution of focal adhesions as well as the reorganization of F-actin were affected by the expression of miR-9-5p. Collectively, these results demonstrate that miR-9-5p promotes MSC migration by upregulating β-catenin signaling pathway, shedding light on the optimization of MSCs for cell replacement therapy through manipulating the expression level of miR-9-5p. Copyright © 2017 the American Physiological Society.

  11. Planeering kui kaasaegne teos par excellence : kas tulevikku saab välja mõelda? = The plan as a contenporary work par excellence : can the future be made up? / Toomas Tammis

    Index Scriptorium Estoniae

    Tammis, Toomas, 1969-

    2011-01-01

    Tulevikku saab kavandada läbi visioonide, läbi erinevate erialade teadmistest kokku lõimunud loomingulise akti, mis ei saa kunagi olla liiga täpne. Planeering saab olla teatav süsteem, mis suudab lõputult produtseerida väikseid üsna täpselt koha- ja keskkonnatundlikke produkte, jäädes ise pidevasse loomisse ning pooleliolekusse, olles pidevas interaktsioonis ühiskonnaga viimast lõputult monitoorides ja muutes

  12. Spatial-temporal-covariance-based modeling, analysis, and simulation of aero-optics wavefront aberrations.

    Science.gov (United States)

    Vogel, Curtis R; Tyler, Glenn A; Wittich, Donald J

    2014-07-01

    We introduce a framework for modeling, analysis, and simulation of aero-optics wavefront aberrations that is based on spatial-temporal covariance matrices extracted from wavefront sensor measurements. Within this framework, we present a quasi-homogeneous structure function to analyze nonhomogeneous, mildly anisotropic spatial random processes, and we use this structure function to show that phase aberrations arising in aero-optics are, for an important range of operating parameters, locally Kolmogorov. This strongly suggests that the d5/3 power law for adaptive optics (AO) deformable mirror fitting error, where d denotes actuator separation, holds for certain important aero-optics scenarios. This framework also allows us to compute bounds on AO servo lag error and predictive control error. In addition, it provides us with the means to accurately simulate AO systems for the mitigation of aero-effects, and it may provide insight into underlying physical processes associated with turbulent flow. The techniques introduced here are demonstrated using data obtained from the Airborne Aero-Optics Laboratory.

  13. Fault Diagnosis of Demountable Disk-Drum Aero-Engine Rotor Using Customized Multiwavelet Method

    Directory of Open Access Journals (Sweden)

    Jinglong Chen

    2015-10-01

    Full Text Available The demountable disk-drum aero-engine rotor is an important piece of equipment that greatly impacts the safe operation of aircraft. However, assembly looseness or crack fault has led to several unscheduled breakdowns and serious accidents. Thus, condition monitoring and fault diagnosis technique are required for identifying abnormal conditions. Customized ensemble multiwavelet method for aero-engine rotor condition identification, using measured vibration data, is developed in this paper. First, customized multiwavelet basis function with strong adaptivity is constructed via symmetric multiwavelet lifting scheme. Then vibration signal is processed by customized ensemble multiwavelet transform. Next, normalized information entropy of multiwavelet decomposition coefficients is computed to directly reflect and evaluate the condition. The proposed approach is first applied to fault detection of an experimental aero-engine rotor. Finally, the proposed approach is used in an engineering application, where it successfully identified the crack fault of a demountable disk-drum aero-engine rotor. The results show that the proposed method possesses excellent performance in fault detection of aero-engine rotor. Moreover, the robustness of the multiwavelet method against noise is also tested and verified by simulation and field experiments.

  14. Acute damage by naphthalene triggers expression of the neuroendocrine marker PGP9.5 in airway epithelial cells

    DEFF Research Database (Denmark)

    Poulsen, T.T.; Naizhen, X.; Linnoila, R.I.

    2008-01-01

    Protein Gene Product 9.5 (PGP9.5) is highly expressed in nervous tissue. Recently PGP9.5 expression has been found to be upregulated in the pulmonary epithelium of smokers and in non-small cell lung cancer, suggesting that it also plays a role in carcinogen-inflicted lung epithelial injury...... neuroendocrine markers was found in the non-neuroendocrine epithelial cells after naphthalene exposure. In contrast, immunostaining for the cell cycle regulator p27(Kip1), which has previously been associated with PGP9.5 in lung cancer cells, revealed transient downregulation of p27(Kip1) in naphthalene exposed...... and further strengthens the accumulating evidence of PGP9.5 as a central player in lung epithelial damage and early carcinogenesis Udgivelsesdato: 2008/9/26...

  15. 75 FR 67639 - Airworthiness Directives; Piaggio Aero Industries S.p.A Model PIAGGIO P-180 Airplanes

    Science.gov (United States)

    2010-11-03

    ... Friday, except Federal holidays. For service information identified in this proposed AD, contact Piaggio... Piaggio Aero Industries have issued service information (referred to after this as ``the MCAI''), to... Information Piaggio Aero Industries S.p.A. has issued Service Bulletin (Mandatory) N.: SB 80-0275, Rev. N. 0...

  16. Numerical Investigation on Windback Seals Used in Aero Engines

    Directory of Open Access Journals (Sweden)

    Michael Flouros

    2018-01-01

    Full Text Available Seals are considered one of the most important flow elements in turbomachinery applications. The most traditional and widely known seal is the labyrinth seal but in recent years other types like the brush or carbon seals were introduced since they considerably reduce the sealing air consumption. When seals are used for sealing of aero engine bearing chambers they are subjected to high “bombardment” through oil particles which are present in the bearing chamber. These particles mainly result from the bearings as a consequence of the high rotational speeds. Particularly when carbon or brush seals are used, problems with carbon formation (coking may arise when oil gets trapped in the very tight gap of these seals. In order to prevent oil migration into the turbomachinery, particularly when the pressure difference over a seal is small or even negligible, significant improvement can be achieved through the introduction of so called windback seals. This seal has a row of static helical teeth (thread and below this thread a scalloped or smooth shaft section is rotating. Depending on the application, a windback seal can be used alone or as a combination with another seal (carbon, brush or labyrinth seal. A CFD analysis carried out with ANSYS CFX version 11 is presented in this paper with the aim to investigate this seal type. The simulations were performed by assuming a two-phase flow of air and oil in the bearing compartment. Design parameters like seal clearance, thread size, scallop width, were investigated at different operating conditions.

  17. SFC Optimization for Aero Engine Based on Hybrid GA-SQP Method

    Science.gov (United States)

    Li, Jie; Fan, Ding; Sreeram, Victor

    2013-12-01

    This study focuses on on-line specific fuel consumption (SFC) optimization of aero engines. For solving this optimization problem, a nonlinear pneumatic and thermodynamics model of the aero engine is built and a hybrid optimization technique which is formed by combining the genetic algorithm (GA) and the sequential quadratic programming (SQP) is presented. The ability of standard GA and standard SQP in solving this type of problem is investigated. It has been found that, although the SQP is fast, very little SFC reductions can be obtained. The GA is able to solve the problem well but a lot of computational time is needed. The presented hybrid GA-SQP gives a good SFC optimization effect and saves 76.6% computational time when compared to the standard GA. It has been shown that the hybrid GA-SQP is a more effective and higher real-time method for SFC on-line optimization of the aero engine.

  18. High-Temperature Adhesives for Thermally Stable Aero-Assist Technologies

    Science.gov (United States)

    Eberts, Kenneth; Ou, Runqing

    2013-01-01

    Aero-assist technologies are used to control the velocity of exploration vehicles (EVs) when entering Earth or other planetary atmospheres. Since entry of EVs in planetary atmospheres results in significant heating, thermally stable aero-assist technologies are required to avoid the high heating rates while maintaining low mass. Polymer adhesives are used in aero-assist structures because of the need for high flexibility and good bonding between layers of polymer films or fabrics. However, current polymer adhesives cannot withstand temperatures above 400 C. This innovation utilizes nanotechnology capabilities to address this need, leading to the development of high-temperature adhesives that exhibit high thermal conductivity in addition to increased thermal decomposition temperature. Enhanced thermal conductivity will help to dissipate heat quickly and effectively to avoid temperature rising to harmful levels. This, together with increased thermal decomposition temperature, will enable the adhesives to sustain transient high-temperature conditions.

  19. "Vedes päi elo tulob..." = "Veest saab elu alguse..." : [luuletused] / Miikul Pahomov ; tlk. Jaan Õispuu

    Index Scriptorium Estoniae

    Pahomov, Miikul

    2006-01-01

    Sisu: "Vedes päi elo tulob..." = "Veest saab elu alguse..." ; "Ei skuup voi pajatada denguush..." = "Ei kooner rahast laulda või..." ; "Coma neicud lyydilaane..." = "Kaunis neiu, lüüdi neiu..." ; "Olizhbo purjeh..." = "Oleks puri mul..." ; "Mi om meiden lyhyd elo..." = "Mis on meie pisku elu..." ; "Sinizhed lindud..." = "Sinised linnud..." ; "Ole, kaivo, puhtaz..." = "Ole, allik, puhas..." ; "Pimedas..." = "Pimedas..." ; Ken miä olen? = Kes ma olen ; Lüüdiland = Lüüdiland ; "Sa kuna mäned, minun rahvaz..." = "Kuhu lähed sa, minu rahvas..." ; Minu kibu - minun mua = Minu valu on minu maa ; Lüüdikiel̀ = Lüüdi keel ; Dälgmäizhed = Viimased ; Kand da latv = Känd ja latv ; Kardàlaine külü = Karjala saun ; Petruskoi = Petruskoi ; "Tägä Suomen taivhan al..." = "Siinse soome taeva all..." ; Viiburin - Piiterin tiel = Viiburi - Piiteri teel

  20. Problems of Aero-optics and Adaptive Optical Systems: Analytical Review

    Directory of Open Access Journals (Sweden)

    Yu. I. Shanin

    2017-01-01

    Full Text Available The analytical review gives the basic concepts of the aero-optics problem arising from the radiation propagation in the region of the boundary layers of a laser installation carrier aircraft. Estimates the radiation wave front distortions at its propagation in the near and far field. Presents main calculation approaches and methods to solve the gas-dynamic and optical problems in propagating laser radiation. Conducts a detailed analysis of the flows and their generating optical aberrations introduced by the aircraft turret (a projection platform of the on-board laser. Considers the effect of various factors (shock wave, difference in wall and flow temperatures on the flow pattern and the optical aberrations. Provides research data on the aero-optics obtained in the flying laboratory directly while in flight. Briefly considers the experimental research methods, diagnostic equipment, and synthesis of results while studying the aero-optics problem. Discusses some methods for mitigating the aerodynamic effects on the light propagation under flight conditions. Presents data about the passive, active, and hybrid effects on the flow in the boundary layers in order to reduce aberrations through improving the flow aerodynamics.The paper considers operation of adaptive optical systems under conditions of aero-optical distortions. Presents the study results concerning the reduction of the aero-optics effect on the characteristics of radiation in far field. Gives some research results regarding the effect on the efficiency of the adaptive system of a laser beam jitter and a time delay in the feedback signal transmission, which occur under application conditions. Provides data on adaptive correction of aero-optical wave fronts of radiation. Considers some application aspects in control systems of the on-board adaptive optics of adaptive filtration as a way to improve the efficiency of adaptive optical systems. The project in mind is to use obtained results

  1. Aero-MINE (Motionless INtegrated Energy) for Distributed Scalable Wind Power.

    Energy Technology Data Exchange (ETDEWEB)

    Houchens, Brent C. [Lawrence Livermore National Lab. (LLNL), Livermore, CA (United States); Blaylock, Myra L. [Lawrence Livermore National Lab. (LLNL), Livermore, CA (United States)

    2017-06-01

    The proposed Aero-MINE technology will extract energy from wind without any exterior moving parts. Aero-MINEs can be integrated into buildings or function stand-alone, and are scalable. This gives them advantages similar to solar panels, but with the added benefit of operation in cloudy or dark conditions. Furthermore, compared to solar panels, Aero-MINEs can be manufactured at lower cost and with less environmental impact. Power generation is isolated internally by the pneumatic transmission of air and the outlet air-jet nozzles amplify the effectiveness. Multiple units can be connected to one centrally located electric generator. Aero-MINEs are ideal for the built-environment, with numerous possible configurations ranging from architectural integration to modular bolt-on products. Traditional wind turbines suffer from many fundamental challenges. The fast-moving blades produce significant aero-acoustic noise, visual disturbances, light-induced flickering and impose wildlife mortality risks. The conversion of massive mechanical torque to electricity is a challenge for gears, generators and power conversion electronics. In addition, the installation, operation and maintenance of wind turbines is required at significant height. Furthermore, wind farms are often in remote locations far from dense regions of electricity customers. These technical and logistical challenges add significantly to the cost of the electricity produced by utility-scale wind farms. In contrast, distributed wind energy eliminates many of the logistical challenges. However, solutions such as micro-turbines produce relatively small amounts of energy due to the reduction in swept area and still suffer from the motion-related disadvantages of utility-scale turbines. Aero-MINEs combine the best features of distributed generation, while eliminating the disadvantages.

  2. Concept of the aero-train and its aerodynamic stability nature

    OpenAIRE

    Kohama, Yasuaki P.; Watanabe, Hideo; Kikuchi, Satoshi; Ota, Fukuo; Ito, Takatoshi; 小濱 泰昭; 渡部 英夫; 菊池 聡; 太田 福雄; 伊藤 高敏

    2000-01-01

    Taking into account the serious greenhouse effect of the earth, drastic proposal which prevents the carbon dioxide emission from transportation system must be done. In Japan, over 20 percent of the carbon dioxide are emitted from transportation. Aero-train is the new zero-emission high speed vehicle, which is being proposed. Wing in ground effect is introduced to obtain highest lift to drag ratio and highest payload ratio. In order to compare the performance of the aero-train at 500 km/h, wit...

  3. Identified state-space prediction model for aero-optical wavefronts

    Science.gov (United States)

    Faghihi, Azin; Tesch, Jonathan; Gibson, Steve

    2013-07-01

    A state-space disturbance model and associated prediction filter for aero-optical wavefronts are described. The model is computed by system identification from a sequence of wavefronts measured in an airborne laboratory. Estimates of the statistics and flow velocity of the wavefront data are shown and can be computed from the matrices in the state-space model without returning to the original data. Numerical results compare velocity values and power spectra computed from the identified state-space model with those computed from the aero-optical data.

  4. Protective role for miR-9-5p in the fibrogenic transformation of human dermal fibroblasts.

    Science.gov (United States)

    Miguel, Verónica; Busnadiego, Oscar; Fierro-Fernández, Marta; Lamas, Santiago

    2016-01-01

    Excessive accumulation of extracellular matrix (ECM) proteins is the hallmark of fibrotic diseases, including skin fibrosis. This response relies on the activation of dermal fibroblasts that evolve into a pro-fibrogenic phenotype. One of the major players in this process is the cytokine transforming growth factor-β (TGF-β). MicroRNAs (miRNAs) are small non-coding RNAs that post-transcriptionally regulate gene expression affecting a wide range of pathophysiological events including fibrogenesis. MicroRNA-9-5p (miR-9-5p) has been shown to exert a protective role in lung and peritoneal fibrosis. This study aimed to evaluate the role of miR-9-5p in skin fibrosis. miR-9-5p is up-regulated in TGF-β1-treated human dermal fibroblasts (HDFs). In silico identification of miR-9-5p targets spotted the type II TGF-β receptor (TGFBR2) as a potential TGF-β signaling-related effector for this miRNA. Consistently, over-expression of miR-9-5p in HDFs down-regulated TGFBR2 at both the mRNA and protein levels and reduced the phosphorylation of Smad2 and the translocation of Smad2/3 to the nucleus. In keeping, over-expression of miR-9-5p significantly delayed TGF-β1-dependent transformation of dermal fibroblasts, decreasing the expression of ECM protein collagen, type I, alpha 1 (Col1α1), and fibronectin (FN), the amount of secreted collagen proteins, and the expression of the archetypal myofibroblast marker alpha-smooth muscle actin (α-SMA). By contrast, specific inhibition of miR-9-5p resulted in enhanced presence of fibrosis markers. The expression of miR-9-5p was also detected in the skin and plasma in the mouse model of bleomycin-induced dermal fibrosis. Using lentiviral constructs, we demonstrated that miR-9-5p over-expression was also capable of deterring fibrogenesis in this same model. miR-9-5p significantly prevents fibrogenesis in skin fibrosis. This is mediated by an abrogation of TGF-β-mediated signaling through the down-regulation of TGFBR2 expression in HDFs

  5. System Aero-Accelator for the purification of biodegradable effluents; Sistema aero-accelator para la depuracion de efluentes biodegradables (I)

    Energy Technology Data Exchange (ETDEWEB)

    Bosque Hernandez, J. L. del; Martin Sanchez, J. L. [Universidad de Salamanca (Spain)

    2000-07-01

    The contamination of the waters is one of the factors that contributes to the deterioration of our environment and since it is a very limited one its treatment descontaminant it is one of the politic's main objectives and environmental administration at all the levels, being spread to the total purification of the generated residual effluents. To reach this objective, big technological efforts are required that allow next to the creation of new processes, the adaptation of the processes existent depuratives, increasing the effectiveness of the same ones. One of the techniques of purification of possible recovery is the Compact System of active mires Aero-Accelator. Presently work is designed and it builds a plant pilot with Aero-Accelator geometry to study its behavior in the treatment of effluents of urban type with different loads pollutants. (Author) 16 refs.

  6. General catalogue of products and services - geology. AERO data base; 2. ed; Catalogo geral de produtos e servicos - geologia. Base de dados AERO

    Energy Technology Data Exchange (ETDEWEB)

    NONE

    1996-12-31

    The catalogue in the second edition aims at presenting to the user a general idea on the aerogeophysical projects of Brazil database (AERO) which belongs to SIGA (Brazilian geological information system). The 151 documents (projects) are listed as follows: 52 projects performed by CPRM/DNPM - Departamento Nacional de Producao Mineral; 33 projects performed by CNEN - Commissao Nacional de Energia Nuclear and NUCLEBRAS; 7 projects executed by State government and private companies; and 59 projects executed for PETROBRAS 159 figs., 5 tabs.

  7. General catalogue of products and services - geology. AERO data base; 2. ed; Catalogo geral de produtos e servicos - geologia. Base de dados AERO

    Energy Technology Data Exchange (ETDEWEB)

    NONE

    1995-12-31

    The catalogue in the second edition aims at presenting to the user a general idea on the aerogeophysical projects of Brazil database (AERO) which belongs to SIGA (Brazilian geological information system). The 151 documents (projects) are listed as follows: 52 projects performed by CPRM/DNPM - Departamento Nacional de Producao Mineral; 33 projects performed by CNEN - Commissao Nacional de Energia Nuclear and NUCLEBRAS; 7 projects executed by State government and private companies; and 59 projects executed for PETROBRAS 159 figs., 5 tabs.

  8. The Application of Advanced Technique of Fan Frame Unit on High Bypass Ratio Aero Engine

    Directory of Open Access Journals (Sweden)

    Hou Peng

    2017-01-01

    Full Text Available High bypass ratio aero-engine was widely used on military and civil aviation domain, as the power of larger aircraft. Fan frame unit was the main bearing frame of high bypass ratio aero-engine, which composed of strut, HUB MID BOX and external bypass parts. Resin/composite was used on external bypass parts(acoustic liner, containment ring, fan outlet guide vane and fan case skin fillets, which not only reduced the weight and manufacturing cost, but also improved the noise absorption, containment and anti-fatigue ability of engine. The design of composite was becoming a key technique for high bypass ratio aero-engine. In special test of the core engine, nitrogen cooling system was designed to cool the cavity of spool. The nitrogen pipeline passed through the inner cavity of fan frame, then inserted into NO. 3 bearing seal, so nitrogen gas was sent into the cavity of core engine spool. On high bypass ratio aero-engine, the external bypass and fan frame inner cavity were the design platform for advanced technique, such as composite and pipeline system, and also provided guarantee for reliable operation of engine.

  9. Performance of small-scale aero-derivative industrial gas turbines derived from helicopter engines

    Directory of Open Access Journals (Sweden)

    Barinyima Nkoi

    2013-12-01

    Full Text Available This paper considers comparative assessment of simple and advanced cycle small-scale aero-derivative industrial gas turbines derived from helicopter engines. More particularly, investigation was made of technical performance of the small-scale aero-derivative engine cycles based on existing and projected cycles for applications in industrial power generation, combined heat and power concept, rotating equipment driving, and/or allied processes. The investigation was done by carrying out preliminary design and performance simulation of a simple cycle (baseline two-spool small-scale aero-derivative turboshaft engine model, and some advanced counterpart aero-derivative configurations. The advanced configurations consist of recuperated and intercooled/recuperated engine cycles of same nominal power rating of 1.567 MW. The baseline model was derived from the conversion of an existing helicopter engine model. In doing so, design point and off-design point performances of the engine models were established. In comparing their performances, it was observed that to a large extent, the advanced engine cycles showed superior performance in terms of thermal efficiency, and specific fuel consumption. In numerical terms, thermal efficiencies of recuperated engine cycle, and intercooled/recuperated engine cycles, over the simple cycle at DP increased by 13.5%, and 14.5% respectively, whereas specific fuel consumption of these cycles over simple cycle at DP decreased by 12.5%, and 13% respectively. This research relied on open access public literature for data.

  10. FJ44 Turbofan Engine Test at NASA Glenn Research Center's Aero-Acoustic Propulsion Laboratory

    Science.gov (United States)

    Lauer, Joel T.; McAllister, Joseph; Loew, Raymond A.; Sutliff, Daniel L.; Harley, Thomas C.

    2009-01-01

    A Williams International FJ44-3A 3000-lb thrust class turbofan engine was tested in the NASA Glenn Research Center s Aero-Acoustic Propulsion Laboratory. This report presents the test set-up and documents the test conditions. Farfield directivity, in-duct unsteady pressures, duct mode data, and phased-array data were taken and are reported separately.

  11. 78 FR 1776 - Airworthiness Directives; International Aero Engines AG Turbofan Engines

    Science.gov (United States)

    2013-01-09

    ... Engines AG Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed... Aero Engines AG (IAE), V2525-D5 and V2528-D5 turbofan engines, with a certain number (No.) 4 bearing... proposed AD. Discussion We received a report of a fire warning on an IAE V2525 turbofan engine shortly...

  12. Aero-Hydro-Elastic Simulation Platform for Wave Energy Systems and floating Wind Turbines

    DEFF Research Database (Denmark)

    Kallesøe, Bjarne Skovmose

    This report present results from the PSO project 2008-1-10092 entitled Aero-Hydro-Elastic Simulation Platform for Wave Energy Systems and floating Wind Turbines that deals with measurements, modelling and simulations of the world’s first combined wave and wind energy platform. The floating energy...

  13. AERO: A Decision Support Tool for Wind Erosion Assessment in Rangelands and Croplands

    Science.gov (United States)

    Galloza, M.; Webb, N.; Herrick, J.

    2015-12-01

    Wind erosion is a key driver of global land degradation, with on- and off-site impacts on agricultural production, air quality, ecosystem services and climate. Measuring rates of wind erosion and dust emission across land use and land cover types is important for quantifying the impacts and identifying and testing practical management options. This process can be assisted by the application of predictive models, which can be a powerful tool for land management agencies. The Aeolian EROsion (AERO) model, a wind erosion and dust emission model interface provides access by non-expert land managers to a sophisticated wind erosion decision-support tool. AERO incorporates land surface processes and sediment transport equations from existing wind erosion models and was designed for application with available national long-term monitoring datasets (e.g. USDI BLM Assessment, Inventory and Monitoring, USDA NRCS Natural Resources Inventory) and monitoring protocols. Ongoing AERO model calibration and validation are supported by geographically diverse data on wind erosion rates and land surface conditions collected by the new National Wind Erosion Research Network. Here we present the new AERO interface, describe parameterization of the underpinning wind erosion model, and provide a summary of the model applications across agricultural lands and rangelands in the United States.

  14. Dependence of AeroMACS Interference on Airport Radiation Pattern Characteristics

    Science.gov (United States)

    Wilson, Jeffrey D.

    2012-01-01

    AeroMACS (Aeronautical Mobile Airport Communications System), which is based upon the IEEE 802.16e mobile wireless standard, is expected to be implemented in the 5091 to 5150 MHz frequency band. As this band is also occupied by Mobile Satellite Service (MSS) feeder uplinks, AeroMACS must be designed to avoid interference with this incumbent service. The aspects of AeroMACS operation that present potential interference are under analysis in order to enable the definition of standards that assure that such interference will be avoided. In this study, the cumulative interference power distribution at low earth orbit from AeroMACS transmitters at the 497 major airports in the contiguous United States was simulated with the Visualyse Professional software. The dependence of the interference power on the number of antenna beams per airport, gain patterns, and beam direction orientations was simulated. As a function of these parameters, the simulation results are presented in terms of the limitations on transmitter power required to maintain the cumulative interference power under the established threshold.

  15. Blades Forced Vibration Under Aero-Elastic Excitation Modeled by Van der Pol

    Czech Academy of Sciences Publication Activity Database

    Půst, Ladislav; Pešek, Luděk

    2017-01-01

    Roč. 27, č. 11 (2017), č. článku 1750166. ISSN 0218-1274 R&D Projects: GA ČR GA16-04546S Institutional support: RVO:61388998 Keywords : ade vibration * aero-elastic force * self-excitation * van der Pol Subject RIV: BI - Acoustics OBOR OECD: Applied mechanics Impact factor: 1.329, year: 2016

  16. Improving Aerospace Engineering Students' Achievements by an Open Aero Control Experiment Apparatus

    Science.gov (United States)

    Zeng, QingHua; Zhang, WeiHua; Huang, ZheZhi; Dong, RongHua

    2014-01-01

    This paper describes the development of an aero control experiment apparatus (ACEA) for use in aerospace control practical courses. The ACEA incorporates a systematic multihierarchy learning and teaching method, and was designed to improve aerospace engineering students' understanding of unmanned aerial vehicle (UAV) control systems. It offers a…

  17. Understanding Aero-Fractures using optics and acoustics

    Science.gov (United States)

    Turkaya, Semih; Toussaint, Renaud; Kvalheim Eriksen, Fredrik; Zecevic, Megan; Daniel, Guillaume; Grude Flekkøy, Eirik; Jørgen Måløy, Knut

    2016-04-01

    exponent p value around 0.5. An analytical model of overpressure diffusion predicting p = 0.5 and two other free parameters of the Omori Law (prefactor and origin time) is developed. The spatial density of the seismic events, and the time of end of formation of the channels can also be predicted using this developed model. Using direct simulations of acoustic emissions due to the air vibration in opening fractal cavities, the evolution in the power spectrum is investigated. 1. Turkaya S, Toussaint R, Eriksen FK, Zecevic M, Daniel G, Flekkøy EG, Måløy KJ. "Bridging aero-fracture evolution with the characteristics of the acoustic emissions in a porous medium." Front. Phys.3:70. 2015 doi: 10.3389/fphy.2015.00070

  18. Smart Rotor Modeling: Aero-Servo-Elastic Modeling of a Smart Rotor with Adaptive Trailing Edge Flaps

    DEFF Research Database (Denmark)

    Bergami, Leonardo

    the trailing edge flap deflection to actively reduce the fatigue loads on the structure. The performance of the smart rotor configuration and its control algorithms are finally quantified by aero-servo-elastic simulations of the smart rotor turbine operating in a standard turbulent wind field.......This book presents the formulation of an aero-servo-elastic model for a wind turbine rotor equipped with Adaptive Trailing Edge Flaps (ATEF), a smart rotor configuration. As the name suggests, an aero-servo-elastic model consists of three main components: an aerodynamic model, a structural model......, and a control model. The book first presents an engineering type of aerodynamic model that accounts for the dynamic effects of flap deflection. The aerodynamic model is implemented in a Blade Element Momentum framework, and coupled with a multi-body structural model in the aero-servoelastic simulation code HAWC...

  19. Fusing Simulation Results From Multifidelity Aero-servo-elastic Simulators - Application To Extreme Loads On Wind Turbine

    DEFF Research Database (Denmark)

    Abdallah, Imad; Sudret, Bruno; Lataniotis, Christos

    2015-01-01

    Fusing predictions from multiple simulators in the early stages of the conceptual design of a wind turbine results in reduction in model uncertainty and risk mitigation. Aero-servo-elastic is a term that refers to the coupling of wind inflow, aerodynamics, structural dynamics and controls. Fusing...... the response data from multiple aero-servo-elastic simulators could provide better predictive ability than using any single simulator. The co-Kriging approach to fuse information from multifidelity aero-servo-elastic simulators is presented. We illustrate the co-Kriging approach to fuse the extreme flapwise...... bending moment at the blade root of a large wind turbine as a function of wind speed, turbulence and shear exponent in the presence of model uncertainty and non-stationary noise in the output. The extreme responses are obtained by two widely accepted numerical aero-servo-elastic simulators, FAST...

  20. Response types and general stability conditions of linear aero-elastic system with two degrees-of-freedom

    Czech Academy of Sciences Publication Activity Database

    Náprstek, Jiří; Pospíšil, Stanislav

    2012-01-01

    Roč. 111, č. 1 (2012), s. 1-13 ISSN 0167-6105 R&D Projects: GA ČR(CZ) GA103/09/0094; GA AV ČR(CZ) IAA200710902 Institutional support: RVO:68378297 Keywords : aero-elastic system * self-excited vibration * instability * aero-elastic derivatives Subject RIV: JN - Civil Engineering Impact factor: 1.342, year: 2012

  1. Global Mobile Satellite Service Interference Analysis for the AeroMACS

    Science.gov (United States)

    Wilson, Jeffrey D.; Apaza, Rafael D.; Hall, Ward; Phillips, Brent

    2013-01-01

    The AeroMACS (Aeronautical Mobile Airport Communications System), which is based on the IEEE 802.16-2009 mobile wireless standard, is envisioned as the wireless network which will cover all areas of airport surfaces for next generation air transportation. It is expected to be implemented in the 5091-5150 MHz frequency band which is also occupied by mobile satellite service uplinks. Thus the AeroMACS must be designed to avoid interference with this incumbent service. Simulations using Visualyse software were performed utilizing a global database of 6207 airports. Variations in base station and subscriber antenna distribution and gain pattern were examined. Based on these simulations, recommendations for global airport base station and subscriber antenna power transmission limitations are provided.

  2. Stille wird zu Farben : [aus "Vaikus saab värvideks" ("Stille wird zu Farben")] : [luuletused] / Jaan Kaplinski ; tlk. Irja Grönholm ja Gisbert Jänicke

    Index Scriptorium Estoniae

    Kaplinski, Jaan, 1941-

    2006-01-01

    Sisu: Stille wird zu Farben ; Der letzte rote Apfel ; Wer allein bleibt ; Ruf nach dem Vorherigen ; Mit jedem Frühling ; So viele Namen ; In die Spuren ; Höher ; Es wird Licht ; Mit dem Sommerwrind um die Wette ; Ob sie noch hört. Orig.: Vaikus saab värvideks ; Viimane verev õun ; Üksi jääb ; Hüüab eelmist ; Iga kevadega ; Niipalju nimesid ; Astub tuule jälgedele ; Käib kõrgemalt ; Saab valguseks ; Suvetuulega võidu ; Kas kuuleb enam

  3. Multimedia in physics education: teaching videos about aero and fluid dynamics

    International Nuclear Information System (INIS)

    Wagner, Andreas; Altherr, Stefan; Eckert, Bodo; Jodl, Hans Joerg

    2007-01-01

    In a series of letters, we present teaching videos on topics which are difficult to understand for students, or which are difficult to realize experimentally in school, if at all. These videos can be used for quantitative analysis or visualization of phenomena. Here we present videos on aero and fluid dynamics which deal with the Navier-Stokes equation, the continuity equation and Karman's vortex street. (letters and comments)

  4. Qualification of Indigenously Developed Special Coatings for Aero-Engine Components

    OpenAIRE

    V. Sambasiva Rao; T. Rangaraju; V. Unnikrishnan

    1999-01-01

    The demand for higher performance and reliability of aero-engiaes necessitates its components to worksatisfactorily under severe operating conditions. The durability of various components in these environmentis often enhanced by applying suitable coatings. The development of new materials/processing methods andalso various coatings to protect the components have been driven by the ever-increasing severity of theaero-engine internal environment. While the selection of a coating is dictated by ...

  5. 76 FR 82202 - Airworthiness Directives; International Aero Engines AG Turbofan Engines

    Science.gov (United States)

    2011-12-30

    ... Engines AG Turbofan Engines AGENCY: Federal Aviation Administration (FAA), DOT. ACTION: Notice of proposed... International Aero Engines AG (IAE) V2500-A1, V2525-D5 and V2528-D5 turbofan engines, and certain serial numbers (S/Ns) of IAE V2522-A5, V2524-A5, V2527-A5, V2527E-A5, V2527M-A5, V2530-A5, and V2533-A5 turbofan...

  6. Results of a WINGDES2/AERO2S Flap Optimization for the TCA

    Science.gov (United States)

    Yaros, Steven F.

    1999-01-01

    The codes WINGDES2 and AERO2S were easy to obtain, and technical help was readily available. The codes have a long, well-documented history of successful optimizations of various aircraft configurations. The codes were easy to use, although specification of input data was time-consuming. The Run times were short, allowing the many runs necessary for the Suction Parameter matrix to be accomplished within a day or two. The results of the optimization appear to be reasonable.

  7. Aero-elastic stability of airfoil flow using 2-D CFD

    Energy Technology Data Exchange (ETDEWEB)

    Johansen, J [Risoe National Lab., Roskilde (Denmark)

    1999-03-01

    A three degrees-of-freedom structural dynamics model has been coupled to a two-dimensional incompressible CFD code. The numerical investigation considers aero-elastic stability for two different airfoils; the NACA0012 and the LM 2 18 % airfoils. Stable and unstable configurations and limit cycle oscillations are predicted in accordance with literature for the first airfoil. An attempt to predict stall induced edge-wise vibrations on a wind turbine airfoil fails using this two-dimensional approach. (au)

  8. Role of offending out-door aero-allergen and CD14 C(-159)T ...

    African Journals Online (AJOL)

    Child- hood-onset and adult-onset of asthma showed significant difference in allergen sensitivity as well as genetic background with respect to CD14 polymorphism. Keywords: Asthma, aero-allergen, skin prick test, total IgE, CD14 gene polymorphism. DOI: https://dx.doi.org/10.4314/ahs.v17i4.18. Cite as: Dutta S, Mondal P, ...

  9. General catalogue of products and services - geology. AERO data base. 2. ed.

    International Nuclear Information System (INIS)

    1995-01-01

    The catalogue in the second edition aims at presenting to the user a general idea on the aerogeophysical projects of Brazil database (AERO) which belongs to SIGA (Brazilian geological information system). The 151 documents (projects) are listed as follows: 52 projects performed by CPRM/DNPM - Departamento Nacional de Producao Mineral; 33 projects performed by CNEN - Commissao Nacional de Energia Nuclear and NUCLEBRAS; 7 projects executed by State government and private companies; and 59 projects executed for PETROBRAS

  10. Practice in multi-disciplinary computing. Transonic aero-structural dynamics of semi-monocoque wing

    International Nuclear Information System (INIS)

    Onishi, Ryoichi; Guo, Zhihong; Kimura, Toshiya; Iwamiya, Toshiyuki

    2000-01-01

    Japan Atomic Energy Research Institute is currently involved in expanding the application areas of its distributed parallel computing facility. One of the most anticipated areas of applications is multi-disciplinary interaction problem. This paper introduces the status quo of the system for fluid-structural interaction analysis on the institute's parallel computers by exploring multi-disciplinary engineering methodology. Current application is focused on a transonic aero-elastic analysis of a three dimensional wing. The distinctive features of the system are: (1) Simultaneous executions of fluid and structural codes by exploiting distributed-and-parallel processing technologies. (2) Construction of a computational fluid (aero)-structural dynamics model which combines flow-field grid with a wing structure composed of the external surface and the internal reinforcements. The purpose of this paper is to summarize the basic concepts, analytical methods, and their implementations along with the computed aero-structural properties of a swept-back wing at March, 7 flow condition. (author)

  11. Numerical study of aero-excitation of steam-turbine rotor blade self-oscillations

    Science.gov (United States)

    Galaev, S. A.; Makhnov, V. Yu.; Ris, V. V.; Smirnov, E. M.

    2018-05-01

    Blade aero-excitation increment is evaluated by numerical solution of the full 3D unsteady Reynolds-averaged Navier-Stokes equations governing wet steam flow in a powerful steam-turbine last stage. The equilibrium wet steam model was adopted. Blade surfaces oscillations are defined by eigen-modes of a row of blades bounded by a shroud. Grid dependency study was performed with a reduced model being a set of blades multiple an eigen-mode nodal diameter. All other computations were carried out for the entire blade row. Two cases are considered, with an original-blade row and with a row of modified (reinforced) blades. Influence of eigen-mode nodal diameter and blade reinforcing on aero-excitation increment is analyzed. It has been established, in particular, that maximum value of the aero-excitation increment for the reinforced-blade row is two times less as compared with the original-blade row. Generally, results of the study point definitely to less probability of occurrence of blade self-oscillations in case of the reinforced blade-row.

  12. Performance of a Supercritical CO2 Bottoming Cycle for Aero Applications

    Directory of Open Access Journals (Sweden)

    Florian Jacob

    2017-03-01

    Full Text Available By 2050, the evolutionary approach to aero engine research may no longer provide meaningful returns on investment, whereas more radical approaches to improving thermal efficiency and reducing emissions might still prove cost effective. One such radical concept is the addition of a secondary power cycle that utilizes the otherwise largely wasted residual heat in the core engine’s exhaust gases. This could provide additional shaft power. Supercritical carbon dioxide closed-circuit power cycles are currently being investigated primarily for stationary power applications, but their high power density and efficiency, even for modest peak cycle temperatures, makes them credible bottoming cycle options for aero engine applications. Through individual geometric design and performance studies for each of the bottoming cycle’s major components, it was determined that a simple combined cycle aero engine could offer a 1.9% mission fuel burn benefit over a state-of-the-art geared turbofan for the year 2050. However, the even greater potential of more complex systems demands further investigation. For example, adding inter-turbine reheat (ITR to the combined cycle is predicted to significantly improve the fuel burn benefit.

  13. Mapped Chebyshev Pseudo-Spectral Method for Dynamic Aero-Elastic Problem of Limit Cycle Oscillation

    Science.gov (United States)

    Im, Dong Kyun; Kim, Hyun Soon; Choi, Seongim

    2018-05-01

    A mapped Chebyshev pseudo-spectral method is developed as one of the Fourier-spectral approaches and solves nonlinear PDE systems for unsteady flows and dynamic aero-elastic problem in a given time interval, where the flows or elastic motions can be periodic, nonperiodic, or periodic with an unknown frequency. The method uses the Chebyshev polynomials of the first kind for the basis function and redistributes the standard Chebyshev-Gauss-Lobatto collocation points more evenly by a conformal mapping function for improved numerical stability. Contributions of the method are several. It can be an order of magnitude more efficient than the conventional finite difference-based, time-accurate computation, depending on the complexity of solutions and the number of collocation points. The method reformulates the dynamic aero-elastic problem in spectral form for coupled analysis of aerodynamics and structures, which can be effective for design optimization of unsteady and dynamic problems. A limit cycle oscillation (LCO) is chosen for the validation and a new method to determine the LCO frequency is introduced based on the minimization of a second derivative of the aero-elastic formulation. Two examples of the limit cycle oscillation are tested: nonlinear, one degree-of-freedom mass-spring-damper system and two degrees-of-freedom oscillating airfoil under pitch and plunge motions. Results show good agreements with those of the conventional time-accurate simulations and wind tunnel experiments.

  14. Crystal spectroscopy of silicon aero-gel end-caps driven by a dynamic hohlraum on Z

    International Nuclear Information System (INIS)

    Nash, T.J.; Sanford, T.W.L.; Mock, R.C.; Leeper, R.J.; Chandler, G.A.; Bailey, J.E.; McKenney, J.L.; Mehlhorn, T.A.; Seaman, J.F.; McGurn, J.; Schroen, D.; Russell, C.; Lake, P.E.; Jobe, D.O.; Gilliland, T.; Nielsen, D.S.; Lucas, J.; Moore, T.; Torres, J.A.; MacFarlane, J.J.; Apruzese, J.P.; Chrien, R.; Idzorek, G.; Peterson, D.L.; Watt, R.

    2005-01-01

    We present results from crystal spectroscopic analysis of silicon aero-gel foams heated by dynamic hohlraums on Z. The dynamic hohlraum on Z creates a radiation source with a 230-eV average temperature over a 2.4-mm diameter. In these experiments silicon aero-gel foams with 10-mg/cm3 densities and 1.7-mm lengths were placed on both ends of the dynamic hohlraum. Several crystal spectrometers were placed both above and below the z-pinch to diagnose the temperature of the silicon aero-gel foam using the K-shell lines of silicon. The crystal spectrometers were (1) temporally integrated and spatially resolved, (2) temporally resolved and spatially integrated, and (3) both temporally and spatially resolved. The results indicate that the dynamic hohlraum heats the silicon aero-gel to approximately 150-eV at peak power. As the dynamic hohlraum source cools after peak power the silicon aero-gel continues to heat and jets axially at an average velocity of approximately 50-cm/μs. The spectroscopy has also shown that the reason for the up/down asymmetry in radiated power on Z is that tungsten enters the line-of-sight on the bottom of the machine much more than on the top

  15. Level-2 perspectives computed quickly and spontaneously: Evidence from eight- to 9.5-year-old children.

    Science.gov (United States)

    Elekes, Fruzsina; Varga, Máté; Király, Ildikó

    2017-11-01

    It has been widely assumed that computing how a scene looks from another perspective (level-2 perspective taking, PT) is an effortful process, as opposed to the automatic capacity of tracking visual access to objects (level-1 PT). Recently, adults have been found to compute both forms of visual perspectives in a quick but context-sensitive way, indicating that the two functions share more features than previously assumed. However, the developmental literature still shows the dissociation between automatic level-1 and effortful level-2 PT. In the current paper, we report an experiment showing that in a minimally social situation, participating in a number verification task with an adult confederate, eight- to 9.5-year-old children demonstrate similar online level-2 PT capacities as adults. Future studies need to address whether online PT shows selectivity in children as well and develop paradigms that are adequate to test preschoolers' online level-2 PT abilities. Statement of Contribution What is already known on this subject? Adults can access how objects appear to others (level-2 perspective) spontaneously and online Online level-1, but not level-2 perspective taking (PT) has been documented in school-aged children What the present study adds? Eight- to 9.5-year-olds performed a number verification task with a confederate who had the same task Children showed similar perspective interference as adults, indicating spontaneous level-2 PT Not only agent-object relations but also object appearances are computed online by eight- to 9.5-year-olds. © 2017 The British Psychological Society.

  16. Half metallic ferromagnet Pr_0_._9_5Mn_0_._9_3_9O_3 for spin based devices

    International Nuclear Information System (INIS)

    Santhosh Kumar, B.; Praveen Shankar, N.; Venkateswaran, C.; Manimuthu, P.

    2016-01-01

    Half Metallic Ferromagnets (HMF) are excellent candidates for spintronics devices due to their unusual 3d and 4s bands. Band theory and first principles calculations strongly predict that Pr based compounds are promising HMF candidates due to their spin hybridisation. Among all Pr based HMF, Pr_0_._9_5Mn_0_._9_3_9O_3 is special because of its pervoskite structure. The different oxidation states of Mn and Pr will enhance the hybridisation of 3d and 4f bands. The present study is experimental effort on the preparation of Pr based compounds

  17. 75 FR 10694 - Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Models N22B, N22S, and N24A...

    Science.gov (United States)

    2010-03-09

    ... Airworthiness Directives; AeroSpace Technologies of Australia Pty Ltd Models N22B, N22S, and N24A Airplanes... authority for Australia, has issued AD GAF-N22-52, Amendment 1, dated January 2010 (referred to after this... examining the MCAI in the AD docket. Relevant Service Information AeroSpace Technologies of Australia...

  18. Machining the Integral Impeller and Blisk of Aero-Engines: A Review of Surface Finishing and Strengthening Technologies

    Science.gov (United States)

    Fu, Youzhi; Gao, Hang; Wang, Xuanping; Guo, Dongming

    2017-05-01

    The integral impeller and blisk of an aero-engine are high performance parts with complex structure and made of difficult-to-cut materials. The blade surfaces of the integral impeller and blisk are functional surfaces for power transmission, and their surface integrity has significant effects on the aerodynamic efficiency and service life of an aero-engine. Thus, it is indispensable to finish and strengthen the blades before use. This paper presents a comprehensive literature review of studies on finishing and strengthening technologies for the impeller and blisk of aero-engines. The review includes independent and integrated finishing and strengthening technologies and discusses advanced rotational abrasive flow machining with back-pressure used for finishing the integral impeller and blisk. A brief assessment of future research problems and directions is also presented.

  19. Development and Validation of a New Blade Element Momentum Skewed-Wake Model within AeroDyn: Preprint

    Energy Technology Data Exchange (ETDEWEB)

    Ning, S. A.; Hayman, G.; Damiani, R.; Jonkman, J.

    2014-12-01

    Blade element momentum methods, though conceptually simple, are highly useful for analyzing wind turbines aerodynamics and are widely used in many design and analysis applications. A new version of AeroDyn is being developed to take advantage of new robust solution methodologies, conform to a new modularization framework for National Renewable Energy Laboratory's FAST, utilize advanced skewed-wake analysis methods, fix limitations with previous implementations, and to enable modeling of highly flexible and nonstraight blades. This paper reviews blade element momentum theory and several of the options available for analyzing skewed inflow. AeroDyn implementation details are described for the benefit of users and developers. These new options are compared to solutions from the previous version of AeroDyn and to experimental data. Finally, recommendations are given on how one might select from the various available solution approaches.

  20. Aero-medical evacuation from the second Israel-Lebanon war: a descriptive study.

    Science.gov (United States)

    Schwartz, Dagan; Resheff, Avram; Geftler, Alex; Weiss, Aviram; Birenbaum, Erez; Lavon, Ophir

    2009-05-01

    The second Lebanon war started as a limited operation and progressed to a large-scale campaign. Most of the fighting took place in mountainous villages and small towns inhabited with civilians. The Israeli Defense Forces (IDF) Airborne rescue and evacuation unit is charged with air evacuation of soldiers and civilians in times of peace, limited conflict, and war. We describe this unit's activities in the second Lebanon war, analyzing injury, treatment, and evacuation characteristics Data were collected from flight medical reports, debriefings of aero-medical team members (usually immediately upon return from mission), ground units medical reports and debriefings, and hospital records. 725 IDF soldiers were injured and 117 killed either in Lebanon or near the Israeli-Lebanese border during the war. A total of 338 (46%) were evacuated in 95 airlifts (averaging 4.5 evacuees per airlift) from the fighting zones or the border. Air evacuation used dedicated helicopters with advanced care capacities, and most victims were evacuated straight from the battlefield, as the fighting was ensuing. Many wounded first received advanced medical care upon the arrival of the aero-medical teams. In military operations within civilian populated areas with threats to ground transport, air evacuation can sometimes be the only readily available option. Providing timely ground advanced medical care proved difficult in many instances. Thus, for many, the rescue helicopter was the first point of access to such care. Aero-medical aircrafts and personnel faced threats from gunfire and missiles, causing both delays in evacuation and a high average number of evacuees per airlift. This article proposes ways of coping with situations in which similar rescue and evacuation problems are likely.

  1. The spectral analysis of an aero-engine assembly incorporating a squeeze-film damper

    Science.gov (United States)

    Holmes, R.; Dede, M. M.

    1989-01-01

    Aero-engine structures have very low inherent damping and so artificial damping is often introduced by pumping oil into annular gaps between the casings and the outer races of some or all of the rolling-element bearings supporting the rotors. The thin oil films so formed are called squeeze film dampers and they can be beneficial in reducing rotor vibration due to unbalance and keeping to reasonable limits the forces transmitted to the engine casing. However, squeeze-film dampers are notoriously non-linear and as a result can introduce into the assembly such phenomena as subharmonic oscillations, jumps and combination frequencies. The purpose of the research is to investigate such phenomena both theoretically and experimentally on a test facility reproducing the essential features of a medium-size aero engine. The forerunner of this work was published. It was concerned with the examination of a squeeze-film damper in series with housing flexibility when supporting a rotor. The structure represented to a limited extent the essentials of the projected Rolls Royce RB401 engine. That research demonstrated the ability to calculate the oil-film forces arising from the squeeze film from known motions of the bearing components and showed that the dynamics of a shaft fitted with a squeeze film bearing can be predicted reasonably accurately. An aero-engine will normally have at least two shafts and so in addition to the excitation forces which are synchronous with the rotation of one shaft, there will also be forces at other frequencies from other shafts operating on the squeeze-film damper. Theoretical and experimental work to consider severe loading of squeeze-film dampers and to include these additional effects are examined.

  2. Recent trends in superalloys research for critical aero-engine components

    Energy Technology Data Exchange (ETDEWEB)

    Remy, Luc [Mine ParisTech, CNRS UMR 7633, 91 - Evry (France). Centre des Materiaux; Guedou, Jean-Yves [Snecma Safran Group, Moissy-Cramayel (France). Materials and Processes Dept.

    2010-07-01

    This paper is a brief survey of common research activity on superalloys for aero-engines between Snecma and Mines ParisTech Centre des Materiaux during recent years. First in disks applications, the development of new powder metallurgy superalloys is shown. Then grain boundary engineering is investigated in a wrought superalloy. Secondly, design oriented research on single crystals blades is shown: a damage model for low cycle fatigue is used for life prediction when cracks initiated at casting pores. The methodology developed for assessing coating life is illustrated for thermal barrier coating deposited on AMI single crystal superalloy. (orig.)

  3. Statistical learning methods for aero-optic wavefront prediction and adaptive-optic latency compensation

    Science.gov (United States)

    Burns, W. Robert

    Since the early 1970's research in airborne laser systems has been the subject of continued interest. Airborne laser applications depend on being able to propagate a near diffraction-limited laser beam from an airborne platform. Turbulent air flowing over the aircraft produces density fluctuations through which the beam must propagate. Because the index of refraction of the air is directly related to the density, the turbulent flow imposes aberrations on the beam passing through it. This problem is referred to as Aero-Optics. Aero-Optics is recognized as a major technical issue that needs to be solved before airborne optical systems can become routinely fielded. This dissertation research specifically addresses an approach to mitigating the deleterious effects imposed on an airborne optical system by aero-optics. A promising technology is adaptive optics: a feedback control method that measures optical aberrations and imprints the conjugate aberrations onto an outgoing beam. The challenge is that it is a computationally-difficult problem, since aero-optic disturbances are on the order of kilohertz for practical applications. High control loop frequencies and high disturbance frequencies mean that adaptive-optic systems are sensitive to latency in sensors, mirrors, amplifiers, and computation. These latencies build up to result in a dramatic reduction in the system's effective bandwidth. This work presents two variations of an algorithm that uses model reduction and data-driven predictors to estimate the evolution of measured wavefronts over a short temporal horizon and thus compensate for feedback latency. The efficacy of the two methods are compared in this research, and evaluated against similar algorithms that have been previously developed. The best version achieved over 75% disturbance rejection in simulation in the most optically active flow region in the wake of a turret, considerably outperforming conventional approaches. The algorithm is shown to be

  4. AeroPropulsoServoElasticity: Dynamic Modeling of the Variable Cycle Propulsion System

    Science.gov (United States)

    Kopasakis, George

    2012-01-01

    This presentation was made at the 2012 Fundamental Aeronautics Program Technical Conference and it covers research work for the Dynamic Modeling of the Variable cycle Propulsion System that was done under the Supersonics Project, in the area of AeroPropulsoServoElasticity. The presentation covers the objective for the propulsion system dynamic modeling work, followed by the work that has been done so far to model the variable Cycle Engine, modeling of the inlet, the nozzle, the modeling that has been done to model the affects of flow distortion, and finally presenting some concluding remarks and future plans.

  5. Applications of aero-acoustic analysis to wind turbine noise control

    International Nuclear Information System (INIS)

    Lowson, M.V.

    1992-01-01

    Wind turbine noise generation mechanisms are essentially equivalent to the aero-acoustic mechanisms of other rotors, which have been studied in depth for many years. Basic sources for the wind turbine noise radiation process are defined, and their significance assessed. From the analysis, areas of potential improvement in wind turbine noise prediction are defined. Suggestions are made for approaches to wind turbine noise control which separate the noise problems at cut-in from those at rated power. Some of these offer the possibility of noise reduction without unfavourable effects on performance. (author)

  6. Applications of aero-acoustic analysis to wind turbine noise control

    International Nuclear Information System (INIS)

    Lowson, M.

    1993-01-01

    Wind turbine noise generation mechanisms are essentially equivalent to the aero-acoustic mechanisms of other rotors, which have been studied in depth for many years. Basic sources for the wind turbine noise radiation process are defined, and their significance assessed. From the analysis, areas of potential improvement in wind turbine noise prediction are defined. Suggestions are made for approaches to wind turbine noise control which separate the noise problems at cut-in from those at rated power. Some of these offer the possibility of noise reduction without unfavourable effects on performance. (author)

  7. Aero-servo-viscoelasticity theory: Lifting surfaces, plates, velocity transients, flutter, and instability

    Science.gov (United States)

    Merrett, Craig G.

    Modern flight vehicles are fabricated from composite materials resulting in flexible structures that behave differently from the more traditional elastic metal structures. Composite materials offer a number of advantages compared to metals, such as improved strength to mass ratio, and intentional material property anisotropy. Flexible aircraft structures date from the Wright brothers' first aircraft with fabric covered wooden frames. The flexibility of the structure was used to warp the lifting surface for flight control, a concept that has reappeared as aircraft morphing. These early structures occasionally exhibited undesirable characteristics during flight such as interactions between the empennage and the aft fuselage, or control problems with the elevators. The research to discover the cause and correction of these undesirable characteristics formed the first foray into the field of aeroelasticity. Aeroelasticity is the intersection and interaction between aerodynamics, elasticity, and inertia or dynamics. Aeroelasticity is well suited for metal aircraft, but requires expansion to improve its applicability to composite vehicles. The first is a change from elasticity to viscoelasticity to more accurately capture the solid mechanics of the composite material. The second change is to include control systems. While the inclusion of control systems in aeroelasticity lead to aero-servo-elasticity, more control possibilities exist for a viscoelastic composite material. As an example, during the lay-up of carbon-epoxy plies, piezoelectric control patches are inserted between different plies to give a variety of control options. The expanded field is called aero-servo-viscoelasticity. The phenomena of interest in aero-servo-viscoelasticity are best classified according to the type of structure considered, either a lifting surface or a panel, and the type of dynamic stability present. For both types of structures, the governing equations are integral

  8. Comparison of caffeine disposition following administration by oral solution (energy drink) and inspired powder (AeroShot) in human subjects.

    Science.gov (United States)

    Laizure, S Casey; Meibohm, Bernd; Nelson, Kembral; Chen, Feng; Hu, Zhe-Yi; Parker, Robert B

    2017-12-01

    To determine the disposition and effects of caffeine after administration using a new dosage form (AeroShot) that delivers caffeine by inspiration of a fine powder into the oral cavity and compare it to an equivalent dose of an oral solution (energy drink) as the reference standard. Healthy human subjects (n = 17) inspired a 100 mg caffeine dose using the AeroShot device or consumed an energy drink on separate study days. Heart rate, blood pressure and subject assessments of effects were measured over an 8-h period. Plasma concentrations of caffeine and its major metabolites were determined by liquid chromatography-mass spectrometry. Pharmacokinetic, cardiovascular and perceived stimulant effects were compared between AeroShot and energy drink phases using a paired t test and standard bioequivalency analysis. Caffeine disposition was similar after caffeine administration by the AeroShot device and energy drink: peak plasma concentration 1790 and 1939 ng ml -1 , and area under the concentration-time curve (AUC) 15 579 and 17 569 ng ml -1 × h, respectively, but they were not bioequivalent: AeroShot AUC of 80.3% (confidence interval 71.2-104.7%) and peak plasma concentration of 86.3% (confidence interval 62.8-102.8%) compared to the energy drink. Female subjects did have a significantly larger AUC compared to males after consumption of the energy drink. The heart rate and blood pressure were not significantly affected by the 100 mg caffeine dose, and there were no consistently perceived stimulant effects by the subjects using visual analogue scales. Inspiration of caffeine as a fine powder using the AeroShot device produces a similar caffeine profile and effects compared to administration of an oral solution (energy drink). © 2017 The British Pharmacological Society.

  9. Tumor suppressor function of PGP9.5 is associated with epigenetic regulation in prostate cancer--novel predictor of biochemical recurrence after radical surgery.

    Science.gov (United States)

    Mitsui, Yozo; Shiina, Hiroaki; Hiraki, Miho; Arichi, Naoko; Hiraoka, Takeo; Sumura, Masahiro; Honda, Satoshi; Yasumoto, Hiroaki; Igawa, Mikio

    2012-03-01

    The expression level of protein G product 9.5 (PGP9.5) is downregulated because of promoter CpG hypermethylation in several tumors. We speculated that impaired regulation of PGP9.5 through epigenetic pathways is associated with the pathogenesis of prostate cancer. CpG methylation of the PGP9.5 gene was analyzed in cultured prostate cancer cell lines, 226 localized prostate cancer samples from radical prostatectomy cases, and 80 benign prostate hyperplasia (BPH) tissues. Following 5-aza-2'-deoxycytidune treatment, increased PGP9.5 mRNA transcript expression was found in the LNCaP and PC3 cell lines. With bisulfite DNA sequencing, partial methylation of the PGP9.5 promoter was shown in LNCaP whereas complete methylation was found in PC3 cells. After transfection of PGP9.5 siRNA, cell viability was significantly accelerated in LNCaP but not in PC3 cells as compared with control siRNA transfection. Promoter methylation of PGP9.5 was extremely low in only one of 80 BPH tissues, whereas it was found in 37 of 226 prostate cancer tissues. Expression of the mRNA transcript of PGP9.5 was significantly lower in methylation (+) than methylation (-) prostate cancer tissues. Multivariate analysis of biochemical recurrence (BCR) after an radical prostatectomy revealed pT category and PGP9.5 methylation as prognostically relevant. Further stratification with the pT category in addition to methylation status identified a stepwise reduction of BCR-free probability. This is the first clinical and comprehensive study of inactivation of the PGP9.5 gene via epigenetic pathways in primary prostate cancer. CpG methylation of PGP9.5 in primary prostate cancer might become useful as a molecular marker for early clinical prediction of BCR after radical prostatectomy. ©2012 AACR.

  10. The Chaotic Prediction for Aero-Engine Performance Parameters Based on Nonlinear PLS Regression

    Directory of Open Access Journals (Sweden)

    Chunxiao Zhang

    2012-01-01

    Full Text Available The prediction of the aero-engine performance parameters is very important for aero-engine condition monitoring and fault diagnosis. In this paper, the chaotic phase space of engine exhaust temperature (EGT time series which come from actual air-borne ACARS data is reconstructed through selecting some suitable nearby points. The partial least square (PLS based on the cubic spline function or the kernel function transformation is adopted to obtain chaotic predictive function of EGT series. The experiment results indicate that the proposed PLS chaotic prediction algorithm based on biweight kernel function transformation has significant advantage in overcoming multicollinearity of the independent variables and solve the stability of regression model. Our predictive NMSE is 16.5 percent less than that of the traditional linear least squares (OLS method and 10.38 percent less than that of the linear PLS approach. At the same time, the forecast error is less than that of nonlinear PLS algorithm through bootstrap test screening.

  11. Research and Development of Some Advanced High Temperature Titanium Alloys for Aero-engine

    Directory of Open Access Journals (Sweden)

    CAI Jian-ming

    2016-08-01

    Full Text Available Some advanced high temperature titanium alloys are usually selected to be manufactured into blade, disc, case, blisk and bling under high temperature environment in compressor and turbine system of a new generation high thrust-mass ratio aero-engine. The latest research progress of 600℃ high temperature titanium alloy, fireproof titanium alloy, TiAl alloy, continuous SiC fiber reinforced titanium matrix composite and their application technology in recent years in China were reviewed in this paper. The key technologies need to be broken through in design, processing and application of new material and component are put forward, including industrial ingot composition of high purified and homogeneous control technology, preparation technology of the large size bar and special forgings, machining technology of blisk and bling parts, material property evaluation and application design technique. The future with the continuous application of advanced high temperature titanium alloys, will be a strong impetus to the development of China's aero-engine technology.

  12. The Design and Semi-Physical Simulation Test of Fault-Tolerant Controller for Aero Engine

    Science.gov (United States)

    Liu, Yuan; Zhang, Xin; Zhang, Tianhong

    2017-11-01

    A new fault-tolerant control method for aero engine is proposed, which can accurately diagnose the sensor fault by Kalman filter banks and reconstruct the signal by real-time on-board adaptive model combing with a simplified real-time model and an improved Kalman filter. In order to verify the feasibility of the method proposed, a semi-physical simulation experiment has been carried out. Besides the real I/O interfaces, controller hardware and the virtual plant model, semi-physical simulation system also contains real fuel system. Compared with the hardware-in-the-loop (HIL) simulation, semi-physical simulation system has a higher degree of confidence. In order to meet the needs of semi-physical simulation, a rapid prototyping controller with fault-tolerant control ability based on NI CompactRIO platform is designed and verified on the semi-physical simulation test platform. The result shows that the controller can realize the aero engine control safely and reliably with little influence on controller performance in the event of fault on sensor.

  13. Takagi-Sugeno fuzzy model identification for turbofan aero-engines with guaranteed stability

    Directory of Open Access Journals (Sweden)

    Ruichao LI

    2018-06-01

    Full Text Available This paper is concerned with identifying a Takagi-Sugeno (TS fuzzy model for turbofan aero-engines working under the maximum power status (non-afterburning. To establish the fuzzy system, theoretical contributions are made as follows. First, by fixing antecedent parameters, the estimation of consequent parameters in state-space representations is formulated as minimizing a quadratic cost function. Second, to avoid obtaining unstable identified models, a new theorem is proposed to transform the prior-knowledge of stability into constraints. Then based on the aforementioned work, the identification problem is synthesized as a constrained quadratic optimization. By solving the constrained optimization, a TS fuzzy system is identified with guaranteed stability. Finally, the proposed method is applied to the turbofan aero-engine using simulation data generated from an aerothermodynamics component-level model. Results show the identified fuzzy model achieves a high fitting accuracy while stabilities of the overall fuzzy system and all its local models are also guaranteed. Keywords: Constrained optimization, Fuzzy system, Stability, System identification, Turbofan engine

  14. Aero-Propulsion Technology (APT) Task V Low Noise ADP Engine Definition Study

    Science.gov (United States)

    Holcombe, V.

    2003-01-01

    A study was conducted to identify and evaluate noise reduction technologies for advanced ducted prop propulsion systems that would allow increased capacity operation and result in an economically competitive commercial transport. The study investigated the aero/acoustic/structural advancements in fan and nacelle technology required to match or exceed the fuel burned and economic benefits of a constrained diameter large Advanced Ducted Propeller (ADP) compared to an unconstrained ADP propulsion system with a noise goal of 5 to 10 EPNDB reduction relative to FAR 36 Stage 3 at each of the three measuring stations namely, takeoff (cutback), approach and sideline. A second generation ADP was selected to operate within the maximum nacelle diameter constrain of 160 deg to allow installation under the wing. The impact of fan and nacelle technologies of the second generation ADP on fuel burn and direct operating costs for a typical 3000 nm mission was evaluated through use of a large, twin engine commercial airplane simulation model. The major emphasis of this study focused on fan blade aero/acoustic and structural technology evaluations and advanced nacelle designs. Results of this study have identified the testing required to verify the interactive performance of these components, along with noise characteristics, by wind tunnel testing utilizing and advanced interaction rig.

  15. Aftereffect of radiotherapy of upper aero-digestive tracts in odontological care

    International Nuclear Information System (INIS)

    Schiochet, Luc

    2010-01-01

    In its first part, this thesis proposes a detailed presentation of the upper aero-digestive tract cancer. The author defines the cancerous process, describes anatomic aspects, and discusses epidemiological aspects (occurrence, mortality, survival, and epidemiological data in different countries). In the second part, the author discusses the role of radiotherapy and of dental surgery in taking a cancerous patient into care (general principles of radiotherapy, therapeutic options and choices, association of radiotherapy, chemotherapy and surgery). Principles of radiotherapy are then more precisely addressed: physical principles (X rays, gamma rays, electrons, neutrons, and protons), radioactivity doses, radiotherapy effect, main equipment, radiotherapy techniques (conformational or intensity-modulated radiotherapy, computed tomography, Cyberknife, external radiotherapy, brachytherapy). The third part addresses early oral-facial complications induced by radiotherapy: factors favouring these complications, nervous effects, effects on the blood system and on the skin, hyposialia and xerostomia, radio-induced mucositis of upper aero-digestive tracts. The next part addresses late effects: late cutaneous after-effects, late radio-mucositis, limitation of mouth opening, tooth decays, osteoradionecrosis. The last part addresses the role of the dental surgeon in taking into care a patient whose head and neck have been irradiated: role before irradiation, during irradiation, and after irradiation [fr

  16. Fuselage boundary-layer refraction of fan tones radiated from an installed turbofan aero-engine.

    Science.gov (United States)

    Gaffney, James; McAlpine, Alan; Kingan, Michael J

    2017-03-01

    A distributed source model to predict fan tone noise levels of an installed turbofan aero-engine is extended to include the refraction effects caused by the fuselage boundary layer. The model is a simple representation of an installed turbofan, where fan tones are represented in terms of spinning modes radiated from a semi-infinite circular duct, and the aircraft's fuselage is represented by an infinitely long, rigid cylinder. The distributed source is a disk, formed by integrating infinitesimal volume sources located on the intake duct termination. The cylinder is located adjacent to the disk. There is uniform axial flow, aligned with the axis of the cylinder, everywhere except close to the cylinder where there is a constant thickness boundary layer. The aim is to predict the near-field acoustic pressure, and in particular, to predict the pressure on the cylindrical fuselage which is relevant to assess cabin noise. Thus no far-field approximations are included in the modelling. The effect of the boundary layer is quantified by calculating the area-averaged mean square pressure over the cylinder's surface with and without the boundary layer included in the prediction model. The sound propagation through the boundary layer is calculated by solving the Pridmore-Brown equation. Results from the theoretical method show that the boundary layer has a significant effect on the predicted sound pressure levels on the cylindrical fuselage, owing to sound radiation of fan tones from an installed turbofan aero-engine.

  17. A Co-modeling Method Based on Component Features for Mechatronic Devices in Aero-engines

    Science.gov (United States)

    Wang, Bin; Zhao, Haocen; Ye, Zhifeng

    2017-08-01

    Data-fused and user-friendly design of aero-engine accessories is required because of their structural complexity and stringent reliability. This paper gives an overview of a typical aero-engine control system and the development process of key mechatronic devices used. Several essential aspects of modeling and simulation in the process are investigated. Considering the limitations of a single theoretic model, feature-based co-modeling methodology is suggested to satisfy the design requirements and compensate for diversity of component sub-models for these devices. As an example, a stepper motor controlled Fuel Metering Unit (FMU) is modeled in view of the component physical features using two different software tools. An interface is suggested to integrate the single discipline models into the synthesized one. Performance simulation of this device using the co-model and parameter optimization for its key components are discussed. Comparison between delivery testing and the simulation shows that the co-model for the FMU has a high accuracy and the absolute superiority over a single model. Together with its compatible interface with the engine mathematical model, the feature-based co-modeling methodology is proven to be an effective technical measure in the development process of the device.

  18. Impact of Early Nutrition on Body Composition in Children Aged 9.5 Years Born with Extremely Low Birth Weight

    Directory of Open Access Journals (Sweden)

    Sonja Stutte

    2017-02-01

    Full Text Available To evaluate body composition, metabolism and growth as well as their interaction with early nutrition in former extremely low birth weight infants (ELBW, we assessed qualitative and quantitative nutritional intake during initial hospitalization and infantile growth parameters in 61 former ELBW infants with a birth weight <1000 g. In two follow-up exams, physical and biochemical development were measured at 5.7 and at 9.5 years. At the second follow-up, in addition to biochemical reassessment, body composition was analyzed by dual-energy x-ray absorptiometry (DEXA. Protein intake between birth and discharge was associated with weight gain in the first six months of life (r = 0.51; p < 0.01. Weight catch-up preceded height catch-up. Protein intake in early infancy correlated highly significantly with abdominal fat mass (r = 0.49; p < 0.05, but not with lean body mass at 9.5 years (r = 0.30; not significant (n.s.. In contrast to nutrient intake, birth weight was associated with lean body mass (r = 0.433; p < 0.001. Early protein and carbohydrate intake were associated with high-density lipoprotein (HDL-cholesterol, and early catch-up growth correlated with fasting insulin at follow-up. Stepwise linear regression demonstrated that protein intake predicted fat mass (p < 0.05, whereas only gender and birth weight standard deviation score (SDS contributed significantly to lean body mass variation (p < 0.05. Our results suggest an important impact of early nutrient intake on body composition and metabolism in later childhood in ELBW children.

  19. Study on aero-dynamic characteristics of the sloop rig (continued); Sloop ring no kuriki tokusei no ichikaiseki (zoku)

    Energy Technology Data Exchange (ETDEWEB)

    Shinkai, A.; Iyoda, H. [Kyushu University, Fukuoka (Japan). Faculty of Engineering

    1997-09-04

    A numerical simulation method was formerly provided for analyzing aero-dynamic characteristics of sloop rig by the vortex distribution method. For this method, aero-dynamic characteristics of the sloop rib were formulated by treating air flow around sail as a two-dimensional problem and by assuming sail as a membrane. The sloop rig is a yacht for more than two persons, which is the most popular form of rig. A main sail and a jib sheet are fixed on a mast. In this study, the method developed based on the panel method was introduced for analyzing the effects of jib sheet which can control the jib trim angle. Generality of the present aero-dynamic characteristics was enhanced, and problems of the analysis method were extracted through the numerical simulation of a yacht with sloop rig. Influence of the position of fairleader on the aero-dynamic characteristics was qualitatively grasped by considering the effects of jib sheet and by trimming the elevation into ideal one. 6 refs., 11 figs.

  20. 75 FR 22512 - Airworthiness Directives; Piaggio Aero Industries S.p.A. Model PIAGGIO P-180 Airplanes

    Science.gov (United States)

    2010-04-29

    ... Airworthiness Directives; Piaggio Aero Industries S.p.A. Model PIAGGIO P-180 Airplanes AGENCY: Federal Aviation... presence of potential ignition sources such as electrical equipment and connectors. As a consequence, this..., agree with their substance. But we might have found it necessary to use different words from those in...

  1. A study on optimal control of the aero-propulsion system acceleration process under the supersonic state

    Directory of Open Access Journals (Sweden)

    Fengyong Sun

    2017-04-01

    Full Text Available In order to solve the aero-propulsion system acceleration optimal problem, the necessity of inlet control is discussed, and a fully new aero-propulsion system acceleration process control design including the inlet, engine, and nozzle is proposed in this paper. In the proposed propulsion system control scheme, the inlet, engine, and nozzle are simultaneously adjusted through the FSQP method. In order to implement the control scheme design, an aero-propulsion system component-level model is built to simulate the inlet working performance and the matching problems between the inlet and engine. Meanwhile, a stabilizing inlet control scheme is designed to solve the inlet control problems. In optimal control of the aero-propulsion system acceleration process, the inlet is an emphasized control unit in the optimal acceleration control system. Two inlet control patterns are discussed in the simulation. The simulation results prove that by taking the inlet ramp angle as an active control variable instead of being modulated passively, acceleration performance could be obviously enhanced. Acceleration objectives could be obtained with a faster acceleration time by 5%.

  2. 76 FR 7694 - Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

    Science.gov (United States)

    2011-02-11

    ... Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes AGENCY: Federal Aviation... Piaggio service bulletin number specified in the Alternative Methods of Compliance (AMOCs) section is..., except Federal holidays. The AD docket contains this AD, the regulatory evaluation, any comments received...

  3. 76 FR 4056 - Airworthiness Directives; PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P-180 Airplanes

    Science.gov (United States)

    2011-01-24

    ..., is considered the State of Design for PIAGGIO AERO INDUSTRIES S.p.A Model PIAGGIO P- 180 airplanes. A... ensuring that the drain lines of the environmental unit condenser are not clogged. Since AD 2007-24-15... condition described previously is likely to exist or develop in other products of the same type design. AD...

  4. Laiad rehvid ja lõvihääl / Jussa Nieminen, Robert Koistinen, Aimo Niemi

    Index Scriptorium Estoniae

    Nieminen, Jussa

    2011-01-01

    TM võrdleb sportautosid: Alfa Romeo Giulietta Quadrifoglio Verde; Audi R8 GT Replica; Audi A1 1,4 TFSI; BMW 1. seeria M Coupé; Cadillac CTS-V Wagon; Chevrolet Camaro SS A; Citroën DS3 Racing; Ferrari 458 Italia; Hyundai Genesis Coupe; Mazda MX-5 Takara Edition; Mercedes-Benz SLS AMG Edition; Mercedes-Benz CLS 63 AMG; Mini Cooper S Countryman All4; Porsche 911 Turbo S; Porsche Cayman R; Saab 9-5 2,8T Aero XWD; Škoda Fabia RS; Subaru STI Racing; Volkswagen Polo GTI; Volvo V60 T6 R-Design Polestar

  5. Aerosols at the poles: an AeroCom Phase II multi-model evaluation

    Directory of Open Access Journals (Sweden)

    M. Sand

    2017-10-01

    Full Text Available Atmospheric aerosols from anthropogenic and natural sources reach the polar regions through long-range transport and affect the local radiation balance. Such transport is, however, poorly constrained in present-day global climate models, and few multi-model evaluations of polar anthropogenic aerosol radiative forcing exist. Here we compare the aerosol optical depth (AOD at 550 nm from simulations with 16 global aerosol models from the AeroCom Phase II model intercomparison project with available observations at both poles. We show that the annual mean multi-model median is representative of the observations in Arctic, but that the intermodel spread is large. We also document the geographical distribution and seasonal cycle of the AOD for the individual aerosol species: black carbon (BC from fossil fuel and biomass burning, sulfate, organic aerosols (OAs, dust, and sea-salt. For a subset of models that represent nitrate and secondary organic aerosols (SOAs, we document the role of these aerosols at high latitudes.The seasonal dependence of natural and anthropogenic aerosols differs with natural aerosols peaking in winter (sea-salt and spring (dust, whereas AOD from anthropogenic aerosols peaks in late spring and summer. The models produce a median annual mean AOD of 0.07 in the Arctic (defined here as north of 60° N. The models also predict a noteworthy aerosol transport to the Antarctic (south of 70° S with a resulting AOD varying between 0.01 and 0.02. The models have estimated the shortwave anthropogenic radiative forcing contributions to the direct aerosol effect (DAE associated with BC and OA from fossil fuel and biofuel (FF, sulfate, SOAs, nitrate, and biomass burning from BC and OA emissions combined. The Arctic modelled annual mean DAE is slightly negative (−0.12 W m−2, dominated by a positive BC FF DAE in spring and a negative sulfate DAE in summer. The Antarctic DAE is governed by BC FF. We perform sensitivity

  6. Effect of CaO on Hot Workability and Microstructure of Mg-9.5Zn-2Y Alloy

    Science.gov (United States)

    Kwak, Tae-yang; Kim, Daeguen; Yang, Jaehack; Yoon, Young-ok; Kim, Shae K.; Lim, Hyunkyu; Kim, Woo Jin

    Mg-Zn-Y system alloys have been a great interest because Mg-Zn-Y alloys with I-phase exhibited high ductility at room and elevated temperatures. According to our preliminary experiments, the addition of CaO improved strength, but the process window became narrow. Therefore, the aim of current work was to find optimum extrusion conditions for CaO added Mg-Zn-Y alloys by processing maps. The 0.3 wt.% of CaO added Mg-9.5Zn-2Y (Mg95.6Zn3.8Y0.6) alloy was prepared by casting into steel mold and homogenizing. Hot compression test were performed in the Gleeble machine at temperature range of 250-400 °C with various strain rates. The alloys were extruded with a reduction ratio of 20:1. To analyze the microstructure and texture, optical micrograph, scanning electron microscope and electron backscattered diffraction were used. Moreover, we investigated the effects of metallic Ca addition in this alloy to compare with the addition of CaO.

  7. Switching LPV Control with Double-Layer LPV Model for Aero-Engines

    Science.gov (United States)

    Tang, Lili; Huang, Jinquan; Pan, Muxuan

    2017-11-01

    To cover the whole range of operating conditions of aero-engine, a double-layer LPV model is built so as to take into account of the variability due to the flight altitude, Mach number and the rotational speed. With this framework, the problem of designing LPV state-feedback robust controller that guarantees desired bounds on both H_∞ and H_2 performances is considered. Besides this, to reduce the conservativeness caused by a single LPV controller of the whole flight envelope and the common Lyapunov function method, a new method is proposed to design a family of LPV switching controllers. The switching LPV controllers can ensure that the closed-loop system remains stable in the sense of Lyapunov under arbitrary switching logic. Meanwhile, the switching LPV controllers can ensure the parameters change smoothly. The validity and performance of the theoretical results are demonstrated through a numerical example.

  8. Methodologies for predicting the part-load performance of aero-derivative gas turbines

    DEFF Research Database (Denmark)

    Haglind, Fredrik; Elmegaard, Brian

    2009-01-01

    Prediction of the part-load performance of gas turbines is advantageous in various applications. Sometimes reasonable part-load performance is sufficient, while in other cases complete agreement with the performance of an existing machine is desirable. This paper is aimed at providing some guidance...... on methodologies for predicting part-load performance of aero-derivative gas turbines. Two different design models – one simple and one more complex – are created. Subsequently, for each of these models, the part-load performance is predicted using component maps and turbine constants, respectively. Comparisons...... with manufacturer data are made. With respect to the design models, the simple model, featuring a compressor, combustor and turbines, results in equally good performance prediction in terms of thermal efficiency and exhaust temperature as does a more complex model. As for part-load predictions, the results suggest...

  9. Propulsion System Dynamic Modeling of the NASA Supersonic Concept Vehicle for AeroPropulsoServoElasticity

    Science.gov (United States)

    Kopasakis, George; Connolly, Joseph W.; Seiel, Jonathan

    2016-01-01

    A summary of the propulsion system modeling under NASA's High Speed Project (HSP) AeroPropulsoServoElasticity (APSE) task is provided with a focus on the propulsion system for the low-boom supersonic configuration developed by Lockheed Martin and referred to as the N+2 configuration. This summary includes details on the effort to date to develop computational models for the various propulsion system components. The objective of this paper is to summarize the model development effort in this task, while providing more detail in the modeling areas that have not been previously published. The purpose of the propulsion system modeling and the overall APSE effort is to develop an integrated dynamic vehicle model to conduct appropriate unsteady analysis of supersonic vehicle performance. This integrated APSE system model concept includes the propulsion system model, and the vehicle structural aerodynamics model. The development to date of such a preliminary integrated model will also be summarized in this report

  10. Reliability Estimation of Aero-engine Based on Mixed Weibull Distribution Model

    Science.gov (United States)

    Yuan, Zhongda; Deng, Junxiang; Wang, Dawei

    2018-02-01

    Aero-engine is a complex mechanical electronic system, based on analysis of reliability of mechanical electronic system, Weibull distribution model has an irreplaceable role. Till now, only two-parameter Weibull distribution model and three-parameter Weibull distribution are widely used. Due to diversity of engine failure modes, there is a big error with single Weibull distribution model. By contrast, a variety of engine failure modes can be taken into account with mixed Weibull distribution model, so it is a good statistical analysis model. Except the concept of dynamic weight coefficient, in order to make reliability estimation result more accurately, three-parameter correlation coefficient optimization method is applied to enhance Weibull distribution model, thus precision of mixed distribution reliability model is improved greatly. All of these are advantageous to popularize Weibull distribution model in engineering applications.

  11. OC3—Benchmark Exercise of Aero-elastic Offshore Wind Turbine Codes

    Science.gov (United States)

    Passon, P.; Kühn, M.; Butterfield, S.; Jonkman, J.; Camp, T.; Larsen, T. J.

    2007-07-01

    This paper introduces the work content and status of the first international investigation and verification of aero-elastic codes for offshore wind turbines as performed by the "Offshore Code Comparison Collaboration"(OC3) within the "IEA Wind Annex XXIII - Subtask 2". An overview is given on the state-of-the-art of the concerned offshore wind turbine simulation codes. Exemplary results of benchmark simulations from the first phase of the project are presented and discussed while subsequent phases are introduced. Furthermore, the paper discusses areas where differences between the codes have been identified and the sources of those differences, such as the differing theories implemented into the individual codes. Finally, further research and code development needs are presented based on the latest findings from the current state of the project.

  12. A Modular Aero-Propulsion System Simulation of a Large Commercial Aircraft Engine

    Science.gov (United States)

    DeCastro, Jonathan A.; Litt, Jonathan S.; Frederick, Dean K.

    2008-01-01

    A simulation of a commercial engine has been developed in a graphical environment to meet the increasing need across the controls and health management community for a common research and development platform. This paper describes the Commercial Modular Aero Propulsion System Simulation (C-MAPSS), which is representative of a 90,000-lb thrust class two spool, high bypass ratio commercial turbofan engine. A control law resembling the state-of-the-art on board modern aircraft engines is included, consisting of a fan-speed control loop supplemented by relevant engine limit protection regulator loops. The objective of this paper is to provide a top-down overview of the complete engine simulation package.

  13. Presentations from the Aeroelastic Workshop - latest results from AeroOpt

    Energy Technology Data Exchange (ETDEWEB)

    Hartvig Hansen, M. (ed.)

    2011-10-15

    This report contains the slides of the presentations at the Aeroelastic Workshop held at Risoe-DTU for the wind energy industry in Denmark on October 27, 2011. The scientific part of the agenda at this workshop was 1) Detailed and reduced models of dynamic mooring system (Anders M. Hansen). 2) Bend-twist coupling investigation in HAWC2 (Taeseong Kim). 3) Q3UIC - A new aerodynamic airfoil tool including rotational effects (Nestor R. Garcia). 4) Influence of up-scaling on loads, control and aerodynamic modeling (Helge Aa. Madsen). 5) Aerodynamic damping of lateral tower vibrations (Bjarne S. Kallesoee). 6) Open- and closed-loop aeroservoelastic analysis with HAWCStab2 (Morten H. Hansen). 7) Design and test of a thick, flatback, high-lift multielement airfoil (Frederik Zahle). The presented results are mainly obtained in the EUDP project ''Aeroelastic Optimization of MW Wind Turbines (AeroOpt)''. (Author)

  14. The Role of Free-Stream Turbulence on High Pressure Turbine Aero-Thermal Stage Interaction

    Science.gov (United States)

    Kopriva, James Earl

    Turbulence plays an important role on the aero-thermal performance of modern aircraft engine High Pressure Turbines (HPT). The role of the vane wake and passage turbulence on the downstream blade flow field is an important consideration for both performance and durability. Obtaining measurements to fully characterize the flow field can be challenging and costly in an experimental facility. Advances in computational Fluid Dynamic (CFD) modeling and High Performance Computing (HPC) are providing opportunity to close these measurement gaps. In order for CFD to be adopted, methods need to be both accurate and efficient. Meshing approaches must also be able to resolve complex HPT geometry while maintaining quality adequate for scale-resolved simulations. Therefore, the accuracy of executing scale-resolved simulations with a second-order code on a mesh of prisms and tetrahedrals in Fluent is considered. Before execution of the HPT computational study, a building block approach is taken to gain quantified predictive performance in the modeling approach as well as understanding limitations in lower computational cost modeling approaches. The predictive capability for Reynolds Averaged Navier Stokes (RANS), Hybrid Large Eddy Simulation (LES), and wall-resolved LES turbulence modeling approaches are first assessed for a cylinder in cross-flow at a Reynolds number of 2580. The flow condition and simple geometry facilitate a quick turn-around for modeling assessment before moving the HPT vane study at high Reynolds and Mach number conditions. Modeling approaches are then assessed relative to the experimental measurements of Arts and Rouvroit (1992) on a pitch-line HPT uncooled vane at high Mach and Reynolds numbers conditions with low (0-6%) free-stream turbulence. The current unstructured second-order LES approach agrees with experimental data and is found to be within the equivalent experimental uncertainty when compared to the structured high-ordered solver FDL3DI. The

  15. EFFECT OF AERO-/ANAEROBIOSIS ON DECARBOXYLASE ACTIVITY OF SELECTED LACTIC ACID BACTERIA

    Directory of Open Access Journals (Sweden)

    Stanislav Kráčmar

    2010-05-01

    Full Text Available Biogenic amines are undesirable compounds produced in foods mainly through bacterial decarboxylase activity. The aim of this study was to investigate some environmental conditions (particularly aero/anaerobiosis, sodium chloride concentration (0–2% w/w, and amount of lactose (0–1% w/w on the activity of tyrosine decarboxylase enzymes of selected six technological important Lactococcus lactis strains. The levels of parameters tested were chosen according to real situation in fermented dairy products technology (especially cheese-making. Tyramine was determined by the ion-exchange chromatography with post-column ninhydrine derivatization and spectrophotometric detection. Tyrosine decarboxylation occurred during the active growth phase. Under the model conditions used, oxygen availability had influence on tyramine production, anaerobiosis seemed to favour the enzyme activity because all L. lactis strains produced higher tyramine amount. doi:10.5219/43

  16. An AeroCom Assessment of Black Carbon in Arctic Snow and Sea Ice

    Science.gov (United States)

    Jiao, C.; Flanner, M. G.; Balkanski, Y.; Bauer, S. E.; Bellouin, N.; Bernsten, T. K.; Bian, H.; Carslaw, K. S.; Chin, M.; DeLuca, N.; hide

    2014-01-01

    Though many global aerosols models prognose surface deposition, only a few models have been used to directly simulate the radiative effect from black carbon (BC) deposition to snow and sea ice. Here, we apply aerosol deposition fields from 25 models contributing to two phases of the Aerosol Comparisons between Observations and Models (AeroCom) project to simulate and evaluate within-snow BC concentrations and radiative effect in the Arctic. We accomplish this by driving the offline land and sea ice components of the Community Earth System Model with different deposition fields and meteorological conditions from 2004 to 2009, during which an extensive field campaign of BC measurements in Arctic snow occurred. We find that models generally underestimate BC concentrations in snow in northern Russia and Norway, while overestimating BC amounts elsewhere in the Arctic. Although simulated BC distributions in snow are poorly correlated with measurements, mean values are reasonable. The multi-model mean (range) bias in BC concentrations, sampled over the same grid cells, snow depths, and months of measurements, are -4.4 (-13.2 to +10.7) ng/g for an earlier phase of AeroCom models (phase I), and +4.1 (-13.0 to +21.4) ng/g for a more recent phase of AeroCom models (phase II), compared to the observational mean of 19.2 ng/g. Factors determining model BC concentrations in Arctic snow include Arctic BC emissions, transport of extra-Arctic aerosols, precipitation, deposition efficiency of aerosols within the Arctic, and meltwater removal of particles in snow. Sensitivity studies show that the model-measurement evaluation is only weakly affected by meltwater scavenging efficiency because most measurements were conducted in non-melting snow. The Arctic (60-90degN) atmospheric residence time for BC in phase II models ranges from 3.7 to 23.2 days, implying large inter-model variation in local BC deposition efficiency. Combined with the fact that most Arctic BC deposition originates

  17. An AeroCom assessment of black carbon in Arctic snow and sea ice

    Energy Technology Data Exchange (ETDEWEB)

    Jiao, C.; Flanner, M. G.; Balkanski, Y.; Bauer, S. E.; Bellouin, N.; Berntsen, T. K.; Bian, H.; Carslaw, K. S.; Chin, M.; De Luca, N.; Diehl, T.; Ghan, S. J.; Iversen, T.; Kirkevåg, A.; Koch, D.; Liu, X.; Mann, G. W.; Penner, J. E.; Pitari, G.; Schulz, M.; Seland, Ø.; Skeie, R. B.; Steenrod, S. D.; Stier, P.; Takemura, T.; Tsigaridis, K.; van Noije, T.; Yun, Y.; Zhang, K.

    2014-01-01

    Though many global aerosols models prognose surface deposition, only a few models have been used to directly simulate the radiative effect from black carbon (BC) deposition to snow and sea ice. In this paper, we apply aerosol deposition fields from 25 models contributing to two phases of the Aerosol Comparisons between Observations and Models (AeroCom) project to simulate and evaluate within-snow BC concentrations and radiative effect in the Arctic. We accomplish this by driving the offline land and sea ice components of the Community Earth System Model with different deposition fields and meteorological conditions from 2004 to 2009, during which an extensive field campaign of BC measurements in Arctic snow occurred. We find that models generally underestimate BC concentrations in snow in northern Russia and Norway, while overestimating BC amounts elsewhere in the Arctic. Although simulated BC distributions in snow are poorly correlated with measurements, mean values are reasonable. The multi-model mean (range) bias in BC concentrations, sampled over the same grid cells, snow depths, and months of measurements, are -4.4 (-13.2 to +10.7) ng g-1 for an earlier phase of AeroCom models (phase I), and +4.1 (-13.0 to +21.4) ng g-1 for a more recent phase of AeroCom models (phase II), compared to the observational mean of 19.2 ng g-1. Factors determining model BC concentrations in Arctic snow include Arctic BC emissions, transport of extra-Arctic aerosols, precipitation, deposition efficiency of aerosols within the Arctic, and meltwater removal of particles in snow. Sensitivity studies show that the model–measurement evaluation is only weakly affected by meltwater scavenging efficiency because most measurements were conducted in non-melting snow. The Arctic (60–90° N) atmospheric residence time for BC in phase II models ranges from 3.7 to 23.2 days, implying large inter-model variation in local BC deposition efficiency. Combined with

  18. Investigation on flow oscillation modes and aero-acoustics generation mechanism in cavity

    Science.gov (United States)

    Yang, Dang-Guo; Lu, Bo; Cai, Jin-Sheng; Wu, Jun-Qiang; Qu, Kun; Liu, Jun

    2018-05-01

    Unsteady flow and multi-scale vortex transformation inside a cavity of L/D = 6 (ratio of length to depth) at Ma = 0.9 and 1.5 were studied using the numerical simulation method of modified delayed detached eddy simulation (DDES) in this paper. Aero-acoustic characteristics for the cavity at same flow conditions were obtained by the numerical method and 0.6 m by 0.6 m transonic and supersonic wind-tunnel experiments. The analysis on the computational and experimental results indicates that some vortex generates from flow separation in shear-layer over the cavity, and the vortex moves from forward to downward of the cavity at some velocity, and impingement of the vortex and the rear-wall of the cavity occurs. Some sound waves spread abroad to the cavity fore-wall, which induces some new vortex generation, and the vortex sheds, moves and impinges on the cavity rear-wall. New sound waves occur. The research results indicate that sound wave feedback created by the impingement of the shedding-vortices and rear cavity face leads to flow oscillations and noise generation inside the cavity. Analysis on aero-acoustic characteristics inside the cavity is feasible. The simulated self-sustained flow-oscillation modes and peak sound pressure on typical frequencies inside the cavity agree well with Rossiter’s and Heller’s predicated results. Moreover, the peak sound pressure occurs in the first and second flow-oscillation modes and most of sound energy focuses on the low-frequency region. Compared with subsonic speed (Ma = 0.9), aerodynamic noise is more intense at Ma = 1.5, which is induced by compression wave or shock wave in near region of fore and rear cavity face.

  19. Advanced Engineering Methods for Assessing Welding Distortion in Aero-Engine Assemblies

    International Nuclear Information System (INIS)

    Jackson, Kathryn; Darlington, Roger

    2011-01-01

    Welding remains an attractive fabrication method for aero-engine assemblies, offering high production rates and reduced total cost, particularly for large complex assemblies. However, distortion generated during the welding process continues to provide a major challenge in terms of the control of geometric tolerances and residual stress. The welding distortion is influenced by the sequence and position of joints, the clamping configuration and the design of the assembly. For large complex assemblies the range of these options may be large. Hence the use of numerical simulation at an early stage of the product development process is valuable to enable a wide range of these factors to be explored with the aim of minimising welding distortions before production commences, and thereby reducing the product development time. In this paper, a new technique for simulation of welding distortions based on a shrinkage analysis is evaluated for an aero-engine assembly. The shrinkage simulations were built and solved using the ESI Group software Weld Planner. The rapid simulation speed enabled a wide range of welding plans to be explored, leading to recommendations for the fabrication process. The sensitivity of the model to mesh size and material properties is reported. The results of the shrinkage analysis were found to be similar to those of a transient analysis generated using ESI Group software SysWeld. The solution times were found to be significantly lower for the shrinkage analysis than the transient analysis. Hence it has been demonstrated that shrinkage analysis is a valuable tool for exploring the fabrication process of a welded assembly at an early stage of the product development process.

  20. Võidusammas saab kliimaseadme

    Index Scriptorium Estoniae

    2009-01-01

    Tšehhi firma Sans Souci paigaldab Tallinnas Vabadussõja võidusamba sisemusse täiendava kliimaseadme ning alustab samba ristiosa sisse LED-paneelide ja elektrisüsteemi taaspaigaldamist. Suletakse vuugivahed. Garantiiremont peab olema lõpetatud 15. detsembriks

  1. Võidusammas saab uue kliimaseadme

    Index Scriptorium Estoniae

    2009-01-01

    Tallinnasse püstitatud Vabadussõja võidusamba remonttöödest. Monumendi ristiosast eemaldatakse niiskusest kahjustatud valgustussüsteem, suletakse samba vuugivahed ja paigaldatakse täiendav kliimaseade. Töid teostab Tšehhi firma Sans Souci

  2. Kõrgkoolidesse saab astuda internetis

    Index Scriptorium Estoniae

    2006-01-01

    Veebipõhise infosüsteemiga SAIS on ühinenud 12 kõrgkooli : Audentese Ülikool, Estonian Business School, Kaitseväe Ühendatud Õppeasutused, Tallinna Ülikool, Eesti Infotehnoloogia Kolledž, Tallinna Tehnikaülikool, Eesti Kunstiakadeemia, Tartu Tervishoiu Kõrgkool, Tartu Ülikool, Eesti Maaülikool, Tallinna Tervishoiu Kõrgkool ja Eesti-Ameerika Äriakadeemia

  3. Pensioni saab endiselt postkontorist

    Index Scriptorium Estoniae

    2008-01-01

    Veebruaris 2009 jõustuvast seadusemuudatusest pensionide kojukande kohta. Ilmunud ka Virumaa Teataja 28. nov. 2008, lk. 4 ; Koit 27. nov. 2008, lk. 2 ; Vooremaa 27. nov. 2008, lk. 3 ; Järva Teataja 27. nov. 2008, lk. 4 ; Nädaline 27. nov. 2008, lk. 5 ; Lääne Elu 27. nov. 2008, lk. 5 ; Sakala 28. nov. 2008, lk. 5 ; Pärnu Postimees 28. nov. 2008, lk. 18 ; Vooremaa 11. dets. 2008, lk. 2

  4. Direct thermal to electrical energy conversion using 9.5/65/35 PLZT ceramics in the ergodic relaxor phase.

    Science.gov (United States)

    Chin, Thomas K; Lee, Felix Y; McKinley, Ian M; Goljahi, Sam; Lynch, Christopher S; Pilon, Laurent

    2012-11-01

    This paper reports on direct thermal to electrical energy conversion by performing the Olsen cycle on 9.5/65/35 lead lanthanum zirconate titanate (PLZT). The Olsen cycle consists of two isothermal and two isoelectric field processes in the electric displacement versus electric field diagram. It was performed by alternatively dipping the material in hot and cold dielectric fluid baths under specified electric fields. The effects of applied electric field, sample thickness, electrode material, operating temperature, and cycle frequency on the energy and power densities were investigated. A maximum energy density of 637 ± 20 J/L/cycle was achieved at 0.054 Hz with a 250-μm-thick sample featuring Pt electrodes and coated with a silicone conformal coating. The operating temperatures varied between 3°C and 140°C and the electric field was cycled between 0.2 and 6.0 MV/m. A maximum power density of 55 ± 8 W/L was obtained at 0.125 Hz under the same operating temperatures and electric fields. The dielectric strength of the material, and therefore the energy and power densities generated, increased when the sample thickness decreased from 500 to 250 μm. Furthermore, the electrode material was found to have no significant effect on the energy and power densities for samples subject to the same operating temperatures and electric fields. However, samples with electrode material possessing thermal expansion coefficients similar to that of PLZT were capable of withstanding larger temperature swings. Finally, a fatigue test showed that the power generation gradually degraded when the sample was subject to repeated thermoelectrical loading.

  5. C-Band Airport Surface Communications System Standards Development. Phase II Final Report. Volume 2: Test Bed Performance Evaluation and Final AeroMACS Recommendations

    Science.gov (United States)

    Hall, Edward; Magner, James

    2011-01-01

    This report is provided as part of ITT s NASA Glenn Research Center Aerospace Communication Systems Technical Support (ACSTS) contract NNC05CA85C, Task 7: New ATM Requirements-Future Communications, C-Band and L-Band Communications Standard Development and was based on direction provided by FAA project-level agreements for New ATM Requirements-Future Communications. Task 7 included two subtasks. Subtask 7-1 addressed C-band (5091- to 5150-MHz) airport surface data communications standards development, systems engineering, test bed and prototype development, and tests and demonstrations to establish operational capability for the Aeronautical Mobile Airport Communications System (AeroMACS). Subtask 7-2 focused on systems engineering and development support of the L-band digital aeronautical communications system (L-DACS). Subtask 7-1 consisted of two phases. Phase I included development of AeroMACS concepts of use, requirements, architecture, and initial high-level safety risk assessment. Phase II builds on Phase I results and is presented in two volumes. Volume I is devoted to concepts of use, system requirements, and architecture, including AeroMACS design considerations. Volume II (this document) describes an AeroMACS prototype evaluation and presents final AeroMACS recommendations. This report also describes airport categorization and channelization methodologies. The purposes of the airport categorization task were (1) to facilitate initial AeroMACS architecture designs and enable budgetary projections by creating a set of airport categories based on common airport characteristics and design objectives, and (2) to offer high-level guidance to potential AeroMACS technology and policy development sponsors and service providers. A channelization plan methodology was developed because a common global methodology is needed to assure seamless interoperability among diverse AeroMACS services potentially supplied by multiple service providers.

  6. C-Band Airport Surface Communications System Standards Development. Phase II Final Report. Volume 1: Concepts of Use, Initial System Requirements, Architecture, and AeroMACS Design Considerations

    Science.gov (United States)

    Hall, Edward; Isaacs, James; Henriksen, Steve; Zelkin, Natalie

    2011-01-01

    This report is provided as part of ITT s NASA Glenn Research Center Aerospace Communication Systems Technical Support (ACSTS) contract NNC05CA85C, Task 7: New ATM Requirements-Future Communications, C-Band and L-Band Communications Standard Development and was based on direction provided by FAA project-level agreements for New ATM Requirements-Future Communications. Task 7 included two subtasks. Subtask 7-1 addressed C-band (5091- to 5150-MHz) airport surface data communications standards development, systems engineering, test bed and prototype development, and tests and demonstrations to establish operational capability for the Aeronautical Mobile Airport Communications System (AeroMACS). Subtask 7-2 focused on systems engineering and development support of the L-band digital aeronautical communications system (L-DACS). Subtask 7-1 consisted of two phases. Phase I included development of AeroMACS concepts of use, requirements, architecture, and initial high-level safety risk assessment. Phase II builds on Phase I results and is presented in two volumes. Volume I (this document) is devoted to concepts of use, system requirements, and architecture, including AeroMACS design considerations. Volume II describes an AeroMACS prototype evaluation and presents final AeroMACS recommendations. This report also describes airport categorization and channelization methodologies. The purposes of the airport categorization task were (1) to facilitate initial AeroMACS architecture designs and enable budgetary projections by creating a set of airport categories based on common airport characteristics and design objectives, and (2) to offer high-level guidance to potential AeroMACS technology and policy development sponsors and service providers. A channelization plan methodology was developed because a common global methodology is needed to assure seamless interoperability among diverse AeroMACS services potentially supplied by multiple service providers.

  7. Reconstruction of the aero-mixture channels of the pulverized coal plant of the 100MW power plant unit

    Directory of Open Access Journals (Sweden)

    Ivanovic Vladan B.

    2011-01-01

    Full Text Available After the last revitalization of thermal power block of 100 MW in TPP “Kostolac A”, made in the year 2004, during the operation of the plant, pulverized coal deposition often occurred in horizontal sections of the aero-mixture channels. Deposition phenomenon manifested itself in places ahead of spherical compensators in the direction of flow of pulverized coal to the burners, due to unfavorable configuration of these channels. Coal dust deposited in the channels dried and spontaneously combusted, causing numerous damage to channels and its isolation as well as the frequent stoppage of the operation for necessary interventions. The paper presents the original solution of reconstruction of aero-mixture channels which prevented deposition of coal dust and its eventual ignition. In this way the reliability of the mill plant is maximized and higher availability of boiler and block as a whole is achieved.

  8. Aero-structural optimization of wind turbine blades using a reduced set of design load cases including turbulence

    DEFF Research Database (Denmark)

    Sessarego, Matias; Shen, Wen Zhong

    2018-01-01

    Modern wind turbine aero-structural blade design codes generally use a smaller fraction of the full design load base (DLB) or neglect turbulent inflow as defined by the International Electrotechnical Commission standards. The current article describes an automated blade design optimization method...... based on surrogate modeling that includes a very large number of design load cases (DLCs) including turbulence. In the present work, 325 DLCs representative of the full DLB are selected based on the message-passing-interface (MPI) limitations in Matlab. Other methods are currently being investigated, e.......g. a Python MPI implementation, to overcome the limitations in Matlab MPI and ultimately achieve a full DLB optimization framework. The reduced DLB and the annual energy production are computed using the state-of-the-art aero-servo-elastic tool HAWC2. Furthermore, some of the interior dimensions of the blade...

  9. Improvement on Main/backup Controller Switching Device of the Nozzle Throat Area Control System for a Turbofan Aero Engine

    Science.gov (United States)

    Li, Jie; Duan, Minghu; Yan, Maode; Li, Gang; Li, Xiaohui

    2014-06-01

    A full authority digital electronic controller (FADEC) equipped with a full authority hydro-mechanical backup controller (FAHMBC) is adopted as the nozzle throat area control system (NTACS) of a turbofan aero engine. In order to ensure the switching reliability of the main/backup controller, the nozzle throat area control switching valve was improved from three-way convex desktop slide valve to six-way convex desktop slide valve. Simulation results show that, if malfunctions of FAEDC occur and abnormal signals are outputted from FADEC, NTACS will be seriously influenced by the main/backup controller switching in several working states, while NTACS will not be influenced by using the improved nozzle throat area control switching valve, thus the controller switching process will become safer and smoother and the working reliability of this turbofan aero engine is improved by the controller switching device improvement.

  10. CONSIDERATIONS ON ANATOMY AND PHYSIOLOGY OF LYMPH VESSELS OF UPPER AERO DIGESTIVE ORGANS AND CERVICAL SATELLITE LYMPH NODE GROUP.

    Science.gov (United States)

    Ciupilan, Corina; Stan, C I

    2016-01-01

    The almost constant local regional development of the cancers of upper aero digestive organs requires the same special attention to cervical lymph node metastases, as well as to the primary neoplastic burning point. The surgical therapy alone or associated has a mutilating, damaging character, resulting in loss of an organ and function, most of the times with social implications, involving physical distortions with aesthetic consequences, which make the reintegration of the individual into society questionable. The problem of cervical lymph node metastases is vast and complex, reason why we approached several anatomical and physiological aspects of lymph vessels of the aero digestive organs. Among the available elements during treatment, the headquarters of the tumour, its histologic degree, and its infiltrative nature, each of them significantly influences the possibility of developing metastases.

  11. Emergency airway management in critically injured patients: a survey of U.S. aero-medical transport programs.

    Science.gov (United States)

    James, Dorsha N; Voskresensky, Igor V; Jack, Meg; Cotton, Bryan A

    2009-06-01

    Pre-hospital airway management represents the intervention most likely to impact outcomes in critically injured patients. As such, airway management issues dominate quality improvement (QI) reviews of aero-medical programs. The purpose of this study was to evaluate current practice patterns of airway management in trauma among U.S. aero-medical service (AMS) programs. The Association of Air Medical Services (AAMS) Resource Guide from 2005 to 2006 was utilized to identify the e-mail addresses of all directors of U.S. aero-medical transport programs. Program directors from 182 U.S. aero-medical programs were asked to participate in an anonymous, web-based survey of emergency airway management protocols and practices. Non-responders to the initial request were contacted a second time by e-mail. 89 programs responded. 98.9% have rapid sequence intubation (RSI) protocols. 90% use succinylcholine, 70% use long-acting neuromuscular blockers (NMB) within their RSI protocol. 77% have protocols for mandatory in-flight sedation but only 13% have similar protocols for maintenance paralytics. 60% administer long-acting NMB immediately after RSI, 13% after confirmation of neurological activity. Given clinical scenarios, however, 97% administer long-acting NMB to patients with scene and in-flight Glasgow Coma Scale (GCS) of 3, even for brief transport times. The majority of AMS programs have well defined RSI and in-flight sedation protocols, while protocols for in-flight NMB are uncommon. Despite this, nearly all programs administer long-acting NMB following RSI, irrespective of GCS or flight time. Given the impact of in-flight NMB on initial assessment, early intervention, and injury severity scoring, a critical appraisal of current AMS airway management practices appears warranted.

  12. miR-9-5p suppresses pro-fibrogenic transformation of fibroblasts and prevents organ fibrosis by targeting NOX4 and TGFBR2.

    Science.gov (United States)

    Fierro-Fernández, Marta; Busnadiego, Óscar; Sandoval, Pilar; Espinosa-Díez, Cristina; Blanco-Ruiz, Eva; Rodríguez, Macarena; Pian, Héctor; Ramos, Ricardo; López-Cabrera, Manuel; García-Bermejo, Maria Laura; Lamas, Santiago

    2015-10-01

    Uncontrolled extracellular matrix (ECM) production by fibroblasts in response to injury contributes to fibrotic diseases, including idiopathic pulmonary fibrosis (IPF). Reactive oxygen species (ROS) generation is involved in the pathogenesis of IPF. Transforming growth factor-β1 (TGF-β1) stimulates the production of NADPH oxidase 4 (NOX4)-dependent ROS, promoting lung fibrosis (LF). Dysregulation of microRNAs (miRNAs) has been shown to contribute to LF. To identify miRNAs involved in redox regulation relevant for IPF, we performed arrays in human lung fibroblasts exposed to ROS. miR-9-5p was selected as the best candidate and we demonstrate its inhibitory effect on TGF-β receptor type II (TGFBR2) and NOX4 expression. Increased expression of miR-9-5p abrogates TGF-β1-dependent myofibroblast phenotypic transformation. In the mouse model of bleomycin-induced LF, miR-9-5p dramatically reduces fibrogenesis and inhibition of miR-9-5p and prevents its anti-fibrotic effect both in vitro and in vivo. In lung specimens from patients with IPF, high levels of miR-9-5p are found. In omentum-derived mesothelial cells (MCs) from patients subjected to peritoneal dialysis (PD), miR-9-5p also inhibits mesothelial to myofibroblast transformation. We propose that TGF-β1 induces miR-9-5p expression as a self-limiting homeostatic response. © 2015 The Authors.

  13. Turbofan Volume Dynamics Model for Investigations of Aero-Propulso-Servo-Elastic Effects in a Supersonic Commercial Transport

    Science.gov (United States)

    Connolly, Joseph W.; Kopasakis, George; Lemon, Kimberly A.

    2010-01-01

    A turbofan simulation has been developed for use in aero-propulso-servo-elastic coupling studies, on supersonic vehicles. A one-dimensional lumped volume approach is used whereby each component (fan, high-pressure compressor, combustor, etc.) is represented as a single volume using characteristic performance maps and conservation equations for continuity, momentum and energy. The simulation is developed in the MATLAB/SIMULINK (The MathWorks, Inc.) environment in order to facilitate controls development, and ease of integration with a future aero-servo-elastic vehicle model being developed at NASA Langley. The complete simulation demonstrated steady state results that closely match a proposed engine suitable for a supersonic business jet at the cruise condition. Preliminary investigation of the transient simulation revealed expected trends for fuel flow disturbances as well as upstream pressure disturbances. A framework for system identification enables development of linear models for controller design. Utilizing this framework, a transfer function modeling an upstream pressure disturbance s impacts on the engine speed is developed as an illustrative case of the system identification. This work will eventually enable an overall vehicle aero-propulso-servo-elastic model

  14. Integrated approach for stress based lifing of aero gas turbine blades

    Science.gov (United States)

    Abu, Abdullahi Obonyegba

    In order to analyse the turbine blade life, the damage due to the combined thermal and mechanical loads should be adequately accounted for. This is more challenging when detailed component geometry is limited. Therefore, a compromise between the level of geometric detail and the complexity of the lifing method to be implemented would be necessary. This research focuses on how the life assessment of aero engine turbine blades can be done, considering the balance between available design inputs and adequate level of fidelity. Accordingly, the thesis contributes to developing a generic turbine blade lifing method that is based on the engine thermodynamic cycle; as well as integrating critical design/technological factors and operational parameters that influence the aero engine blade life. To this end, thermo-mechanical fatigue was identified as the critical damage phenomenon driving the life of the turbine blade.. The developed approach integrates software tools and numerical models created using the minimum design information typically available at the early design stages. Using finite element analysis of an idealised blade geometry, the approach captures relevant impacts of thermal gradients and thermal stresses that contribute to the thermo-mechanical fatigue damage on the gas turbine blade. The blade life is evaluated using the Neu/Sehitoglu thermo-mechanical fatigue model that considers damage accumulation due to fatigue, oxidation, and creep. The leading edge is examined as a critical part of the blade to estimate the damage severity for different design factors and operational parameters. The outputs of the research can be used to better understand how the environment and the operating conditions of the aircraft affect the blade life consumption and therefore what is the impact on the maintenance cost and the availability of the propulsion system. This research also finds that the environmental (oxidation) effect drives the blade life and the blade coolant

  15. The effects of strain and ploidy on the physiological responses of rainbow trout (Oncorhynchus mykiss) to pH 9.5 exposure.

    Science.gov (United States)

    Thompson, William A; Rodela, Tamara M; Richards, Jeffrey G

    2015-05-01

    We characterized the physiological effects of exposure to pH9.5 on one domesticated and four wild strains of diploid and triploid juvenile rainbow trout (Oncorhynchus mykiss) over two consecutive years. In the first year, 35-70% of the individuals from the wild strains showed a loss of equilibrium (LOE) at 12 h exposure to pH9.5, with all fish from wild strains experiencing a LOE by 48 h. In contrast, trout strains and ploidies. Plasma chloride decreased at 24h exposure in all trout strains and ploidies, but recovered by 72 h. No change was observed in plasma sodium. Overall, our data suggest that the domesticated strain of trout is more tolerant of pH9.5 than the wild strains, but these differences in tolerance cannot be explained by our sub-lethal assessment of ammonia balance or ion regulation. Copyright © 2015 Elsevier Inc. All rights reserved.

  16. Review of modern low emissions combustion technologies for aero gas turbine engines

    Science.gov (United States)

    Liu, Yize; Sun, Xiaoxiao; Sethi, Vishal; Nalianda, Devaiah; Li, Yi-Guang; Wang, Lu

    2017-10-01

    Pollutant emissions from aircraft in the vicinity of airports and at altitude are of great public concern due to their impact on environment and human health. The legislations aimed at limiting aircraft emissions have become more stringent over the past few decades. This has resulted in an urgent need to develop low emissions combustors in order to meet legislative requirements and reduce the impact of civil aviation on the environment. This article provides a comprehensive review of low emissions combustion technologies for modern aero gas turbines. The review considers current high Technologies Readiness Level (TRL) technologies including Rich-Burn Quick-quench Lean-burn (RQL), Double Annular Combustor (DAC), Twin Annular Premixing Swirler combustors (TAPS), Lean Direct Injection (LDI). It further reviews some of the advanced technologies at lower TRL. These include NASA multi-point LDI, Lean Premixed Prevaporised (LPP), Axially Staged Combustors (ASC) and Variable Geometry Combustors (VGC). The focus of the review is placed on working principles, a review of the key technologies (includes the key technology features, methods of realising the technology, associated technology advantages and design challenges, progress in development), technology application and emissions mitigation potential. The article concludes the technology review by providing a technology evaluation matrix based on a number of combustion performance criteria including altitude relight auto-ignition flashback, combustion stability, combustion efficiency, pressure loss, size and weight, liner life and exit temperature distribution.

  17. Propulsion System Dynamic Modeling for the NASA Supersonic Concept Vehicle: AeroPropulsoServoElasticity

    Science.gov (United States)

    Kopasakis, George; Connolly, Joseph; Seidel, Jonathan

    2014-01-01

    A summary of the propulsion system modeling under NASA's High Speed Project (HSP) AeroPropulsoServoElasticity (APSE) task is provided with a focus on the propulsion system for the low-boom supersonic configuration developed by Lockheed Martin and referred to as the N+2 configuration. This summary includes details on the effort to date to develop computational models for the various propulsion system components. The objective of this paper is to summarize the model development effort in this task, while providing more detail in the modeling areas that have not been previously published. The purpose of the propulsion system modeling and the overall APSE effort is to develop an integrated dynamic vehicle model to conduct appropriate unsteady analysis of supersonic vehicle performance. This integrated APSE system model concept includes the propulsion system model, and the vehicle structural-aerodynamics model. The development to date of such a preliminary integrated model will also be summarized in this report.propulsion system dynamics, the structural dynamics, and aerodynamics.

  18. A novel full scale experimental characterization of wind turbine aero-acoustic noise sources - preliminary results

    DEFF Research Database (Denmark)

    Aagaard Madsen, Helge; Bertagnolio, Franck; Fischer, Andreas

    2016-01-01

    of the blade and the noise on the ground in a distance of about one rotor diameter. In total six surface microphones were used to measure the SP at the leading edge (LE) and trailing edge (TE) of the blade. In parallel noise was measured by eight microphones placed on plates on the ground around the turbine......The paper describes a novel full scale experiment on a 500 kW wind turbine with the main objective to characterize the aero-acoustic noise sources. The idea behind the instrumentation is to study the link and correlation between the surface pressure (SP) fluctuations in the boundary layer...... in equidistant angles on a circle with a radius of about one rotor diameter. The data were analyzed in segments of 2.2 s which is the time for one rotor revolution. The spectra for the TE microphones on the suction side of the blade show a characteristic roll-off pattern around a frequency of 600-700 Hz...

  19. New design of a compact aero-robotic drilling end effector: An experimental analysis

    Directory of Open Access Journals (Sweden)

    Shi Zhenyun

    2016-08-01

    Full Text Available This paper presents the development of a normal adjustment cell (NAC in aero-robotic drilling to improve the quality of vertical drilling, by using an intelligent double-eccentric disk normal adjustment mechanism (2-EDNA, a spherical plain bearing and a floating compress module with sensors. After the surface normal vector is calculated based on the laser sensors’ feedback, the 2-EDNA concept is conceived specifically to address the deviation of the spindle from the surface normal at the drilling point. Following the angle calculation, depending on the actual initial position, two precise eccentric disks (PEDs with an identical eccentric radius are used to rotate with the appropriate angles using two high-resolution DC servomotors. The two PEDs will carry the spindle to coincide with the surface normal, keeping the vertex of the drill bit still to avoid repeated adjustment and position compensation. A series of experiments was conducted on an aeronautical drilling robot platform with a precise NAC. The effect of normal adjustment on bore diameter, drilling force, burr size, drilling heat, and tool wear was analyzed. The results validate that using the NAC in robotic drilling results in greatly improved vertical drilling quality and is attainable in terms of intelligence and accuracy.

  20. Dynamic behavior of aero-engine rotor with fusing design suffering blade off

    Directory of Open Access Journals (Sweden)

    Cun WANG

    2017-06-01

    Full Text Available Fan blade off (FBO from a running turbofan rotor will introduce sudden unbalance into the dynamical system, which will lead to the rub-impact, the asymmetry of rotor and a series of interesting dynamic behavior. The paper first presents a theoretical study on the response excited by sudden unbalance. The results reveal that the reaction force of the bearing located near the fan could always reach a very high value which may lead to the crush of ball, journal sticking, high stress on the other components and some other failures to endanger the safety of engine in FBO event. Therefore, the dynamic influence of a safety design named “fusing” is investigated by mechanism analysis. Meantime, an explicit FBO model is established to simulate the FBO event, and evaluate the effectiveness and potential dynamic influence of fusing design. The results show that the fusing design could reduce the vibration amplitude of rotor, the reaction force on most bearings and loads on mounts, but the sudden change of support stiffness induced by fusing could produce an impact effect which will couple with the influence of sudden unbalance. Therefore, the implementation of the design should be considered carefully with optimized parameters in actual aero-engine.

  1. Unusual structure in forsterite glass synthesized by an aero-acoustic levitation technique

    International Nuclear Information System (INIS)

    Kohara, Shinji; Suzuya, Kentaro; Takeuchi, Ken

    2005-01-01

    Forsterite Mg 2 SiO 4 exhibits an orthorhombic structure consisted of two kinds of MgO 6 octahedra. One of them forms edge-sharing ribbons along the [001] direction which are linked by the other kind of edge-sharing MgO 6 octahedra, resulting in a three-dimensional framework. Given only 33.3 mol% of SiO 2 in the material, the SiO 4 tetrahedra are isolated within the framework, sharing the O-O bonds with the common edges of the MgO 6 octahedra. If forsterite can be vitrified, an interesting question concerning the glass structure arises because there is insufficient glass forming SiO 2 to establish the corner-sharing SiO 4 tetrahedral net-work needed in conventional silicate glasses. A bulk Mg 2 SiO 4 glass was synthesized using an aero-acoustic levitation technique and to visualize the short-to intermediate-range structure by a combined high-energy synchrotron x-ray and neutron diffraction and reverse Monte Carlo computer simulation. We found that the role of network former is largely taken on by corner-and edge-sharing ionic magnesium species that adopt 4-, 5- and 6-coordination with oxygen. (author)

  2. Uncertainty of measurement for large product verification: evaluation of large aero gas turbine engine datums

    International Nuclear Information System (INIS)

    Muelaner, J E; Wang, Z; Keogh, P S; Brownell, J; Fisher, D

    2016-01-01

    Understanding the uncertainty of dimensional measurements for large products such as aircraft, spacecraft and wind turbines is fundamental to improving efficiency in these products. Much work has been done to ascertain the uncertainty associated with the main types of instruments used, based on laser tracking and photogrammetry, and the propagation of this uncertainty through networked measurements. Unfortunately this is not sufficient to understand the combined uncertainty of industrial measurements, which include secondary tooling and datum structures used to locate the coordinate frame. This paper presents for the first time a complete evaluation of the uncertainty of large scale industrial measurement processes. Generic analysis and design rules are proven through uncertainty evaluation and optimization for the measurement of a large aero gas turbine engine. This shows how the instrument uncertainty can be considered to be negligible. Before optimization the dominant source of uncertainty was the tooling design, after optimization the dominant source was thermal expansion of the engine; meaning that no further improvement can be made without measurement in a temperature controlled environment. These results will have a significant impact on the ability of aircraft and wind turbines to improve efficiency and therefore reduce carbon emissions, as well as the improved reliability of these products. (paper)

  3. Towards an Aero-Propulso-Servo-Elasticity Analysis of a Commercial Supersonic Transport

    Science.gov (United States)

    Connolly, Joseph W.; Kopasakis, George; Chwalowski, Pawel; Sanetrik, Mark D.; Carlson, Jan-Renee; Silva, Walt A.; McNamara, Jack

    2016-01-01

    This paper covers the development of an aero-propulso-servo-elastic (APSE) model using computational fluid dynamics (CFD) and linear structural deformations. The APSE model provides the integration of the following two previously developed nonlinear dynamic simulations: a variable cycle turbofan engine and an elastic supersonic commercial transport vehicle. The primary focus of this study is to provide a means to include relevant dynamics of a turbomachinery propulsion system into the aeroelastic studies conducted during a vehicle design, which have historically neglected propulsion effects. A high fidelity CFD tool is used here for the integration platform. The elastic vehicle neglecting the propulsion system serves as a comparison of traditional approaches to the APSE results. An overview of the methodology is presented for integrating the propulsion system and elastic vehicle. Static aeroelastic analysis comparisons between the traditional and developed APSE models for a wing tip detection indicate that the propulsion system impact on the vehicle elastic response could increase the detection by approximately ten percent.

  4. Aero-hydro-elastic simulation platform for wave energy systems and floating wind turbines

    Energy Technology Data Exchange (ETDEWEB)

    Kallesoee, B.S.

    2011-01-15

    This report present results from the PSO project 2008-1-10092 entitled Aero-Hydro-Elastic Simulation Platform for Wave Energy Systems and floating Wind Turbines that deals with measurements, modelling and simulations of the world's first combined wave and wind energy platform. The floating energy conversion platform, Poseidon, is owned and operated by Floating Power Plant A/S. The platform has been operating for two test periods; one period where it was operating as a wave energy conversion platform only and one period where the three turbines was mounted and the platform operated as a combined wind and wave energy platform. The PSO project has equipped the platform with comprehensive measurements equipment for measuring platform motion, wave and wind conditions and turbine loads. Data from the first test period has been used for determine if the turbine could be mounted on the platform. Preliminary analysis of data from the second test period indicates that the platform is suitable as wind turbine foundation and that the turbines reduce the platform motion. (Author)

  5. AEROS: a real-time emergency response system for atmospheric releases of toxic material

    International Nuclear Information System (INIS)

    Nasstrom, J.S.; Greenly, G.D.

    1986-01-01

    The Atmospheric Release Advisory Capability (ARAC) at the Lawrence Livermore National Laboratory has developed a sophisticated computer-based real-time emergency response system for radiotoxic releases into the atmosphere. The ARAC Emergency Response Operating System (AEROS) has a centralized computer facility linked to remote site computers, meteorological towers, and meteorological data sources. The system supports certain fixed sites, but has the ability to respond to accidents at arbitrary locations. Product quality and response time are optimized by using complex three-dimensional dispersion models; extensive on-line data bases; automated data processing; and an efficient user interface, employing graphical computer displays and computer-displayed forms. Upon notification, the system automatically initiates a response to an emergency and proceeds through preliminary calculations, automatically processing accident information, meteorological data, and model parameters. The model calculations incorporate mass-consistent three-dimensional wind fields, terrain effects, and particle-in-cell diffusion. Model products are color images of dose or deposition contours overlaid on a base map

  6. Aero Engine Component Fault Diagnosis Using Multi-Hidden-Layer Extreme Learning Machine with Optimized Structure

    Directory of Open Access Journals (Sweden)

    Shan Pang

    2016-01-01

    Full Text Available A new aero gas turbine engine gas path component fault diagnosis method based on multi-hidden-layer extreme learning machine with optimized structure (OM-ELM was proposed. OM-ELM employs quantum-behaved particle swarm optimization to automatically obtain the optimal network structure according to both the root mean square error on training data set and the norm of output weights. The proposed method is applied to handwritten recognition data set and a gas turbine engine diagnostic application and is compared with basic ELM, multi-hidden-layer ELM, and two state-of-the-art deep learning algorithms: deep belief network and the stacked denoising autoencoder. Results show that, with optimized network structure, OM-ELM obtains better test accuracy in both applications and is more robust to sensor noise. Meanwhile it controls the model complexity and needs far less hidden nodes than multi-hidden-layer ELM, thus saving computer memory and making it more efficient to implement. All these advantages make our method an effective and reliable tool for engine component fault diagnosis tool.

  7. Cooperating to Compete in the Global Air Cargo Industry: The Case of the DHL Express and Lufthansa Cargo A.G. Joint Venture Airline ‘AeroLogic’

    Directory of Open Access Journals (Sweden)

    Glenn Baxter

    2018-03-01

    Full Text Available This paper presents a case study of the DHL Express and Lufthansa Cargo strategic joint venture cargo airline ‘AeroLogic’, the global air cargo industry’s largest operative joint venture between an airline and a leading international express and logistics provider. The study used a qualitative research approach. The data gathered for the study was examined by document analysis. The strategic analysis of the AeroLogic joint venture was based on the use of Porter’s Five Forces framework. The study found that the AeroLogic joint venture airline has provided synergistic benefits to both partners and has allowed the partners to access new markets and to participate in the evolution of the air cargo industry. The new venture has also enabled both joint venture partners to enhance their competitive position in the global air cargo industry through strengthened service offerings and has provided the partners with increased cargo capacities, a larger route network, and greater frequencies within their own route networks. The study also found that the AeroLogic business model is unique in the air cargo industry. A limitation of the study was that AeroLogic’s annual revenue or freight traffic data was not available. It was, therefore, not possible to analyse the business performance of the joint venture.

  8. Feasibility investigation of coupling a desalination prototype functioning by Aero-Evapo-Condensation with solar units

    International Nuclear Information System (INIS)

    Bourouni, K.; Bouden, C.; Chaibi, M.

    2003-01-01

    The rural regions of south Mediterranean countries suffer from problems of drinking water supply. However, the majority of these regions have important resources of brackish salt water. Thus, brackish water desalination on a small scale presents a potential solution to this problem. For this reason, a number of small desalination prototypes are being developed worldwide. Bourouni et al. have developed a water desalination unit functioning by the Aero-Evapo-Condensation-Process (AECP) in order to satisfy this kind of water demand. One of the advantages of this prototype is that it allows the use of low temperature energy such as geothermal and solar energies abundant in these countries. An initial experiment was carried on an AECP prototype coupled to a geothermal spring in the south of Tunisia. The results relative to the technical and economic performances of the unit have shown that this kind of coupling is promising. On the other hand, the brackish water springs in these countries are often non-geothermal. In this case, the use of solar energy can be considered. Thus, we develop, in the present article, a feasibility investigation on the coupling of the AECP prototype with solar units. In fact, we analyse, in the first part of this article, the possibilities of this coupling in a manner that the functioning mode of the solar units will be compatible with that of the AECP prototype. To attempt this objective, two kinds of solar installation scenarios are considered and modelled to obtain their energetic contribution. Hence, the elaborated models are coupled to the one developed by Bourouni et al. for the AECP prototype to determine the technical and economic performances of the whole installation. In the last part of this article, a solar unit dimensioning is performed in order to minimise the total cost of the distilled water. (author)

  9. Dynamic modeling and vibration characteristics analysis of the aero-engine dual-rotor system with Fan blade out

    Science.gov (United States)

    Yu, Pingchao; Zhang, Dayi; Ma, Yanhong; Hong, Jie

    2018-06-01

    Fan Blade Out (FBO) from a running rotor of the turbofan engine will not only introduce the sudden unbalance and inertia asymmetry into the rotor, but also apply large impact load and induce rotor-to-stator rubbing on the rotor, which makes the mass, gyroscopic and stiffness matrixes of the dynamic equation become time-varying and highly nonlinear, consequently leads to the system's complicated vibration. The dynamic analysis of the aero-engine rotor system is one essential requirement of the authorities and is vital to the aero-engine's safety. The paper aims at studying the dynamic responses of the complicated dual-rotor systems at instantaneous and windmilling statuses when FBO event occurs. The physical process and mechanical characteristics of the FBO event are described qualitatively, based on which the dynamic modeling for an aero-engine dual-rotor system is carried out considering several excitations caused by FBO. Meanwhile the transient response during the instantaneous status and steady-state response at the windmilling status are obtained. The results reveal that the sudden unbalance can induce impact load to the rotor, and lead to the sharp increase of the vibration amplitude and reaction force. The rub-impact will apply constraint effects on the rotor and restrict the transient vibration amplitude, while the inertia asymmetry has little influence on the transient response. When the rotor with huge unbalance operates at windmilling status, the rub-impact turns to be the main factor determining the rotor's dynamic behavior, and several potential motion states, such as instable dry whip, intermittent rubbing and synchronous full annular rubbing would happen on certain conditions.

  10. Small wind turbine performance evaluation using field test data and a coupled aero-electro-mechanical model

    Science.gov (United States)

    Wallace, Brian D.

    A series of field tests and theoretical analyses were performed on various wind turbine rotor designs at two Penn State residential-scale wind-electric facilities. This work involved the prediction and experimental measurement of the electrical and aerodynamic performance of three wind turbines; a 3 kW rated Whisper 175, 2.4 kW rated Skystream 3.7, and the Penn State designed Carolus wind turbine. Both the Skystream and Whisper 175 wind turbines are OEM blades which were originally installed at the facilities. The Carolus rotor is a carbon-fiber composite 2-bladed machine, designed and assembled at Penn State, with the intent of replacing the Whisper 175 rotor at the off-grid system. Rotor aerodynamic performance is modeled using WT_Perf, a National Renewable Energy Laboratory developed Blade Element Momentum theory based performance prediction code. Steady-state power curves are predicted by coupling experimentally determined electrical characteristics with the aerodynamic performance of the rotor simulated with WT_Perf. A dynamometer test stand is used to establish the electromechanical efficiencies of the wind-electric system generator. Through the coupling of WT_Perf and dynamometer test results, an aero-electro-mechanical analysis procedure is developed and provides accurate predictions of wind system performance. The analysis of three different wind turbines gives a comprehensive assessment of the capability of the field test facilities and the accuracy of aero-electro-mechanical analysis procedures. Results from this study show that the Carolus and Whisper 175 rotors are running at higher tip-speed ratios than are optimum for power production. The aero-electro-mechanical analysis predicted the high operating tip-speed ratios of the rotors and was accurate at predicting output power for the systems. It is shown that the wind turbines operate at high tip-speeds because of a miss-match between the aerodynamic drive torque and the operating torque of the wind

  11. PREFACE: The 2nd International Conference on Geological, Geographical, Aerospace and Earth Sciences 2014 (AeroEarth 2014)

    Science.gov (United States)

    Lumban Gaol, Ford; Soewito, Benfano

    2015-01-01

    The 2nd International Conference on Geological, Geographical, Aerospace and Earth Sciences 2014 (AeroEarth 2014), was held at Discovery Kartika Plaza Hotel, Kuta, Bali, Indonesia during 11 - 12 October 2014. The AeroEarth 2014 conference aims to bring together researchers and engineers from around the world. Through research and development, earth scientists have the power to preserve the planet's different resource domains by providing expert opinion and information about the forces which make life possible on Earth. Earth provides resources and the exact conditions to make life possible. However, with the advent of technology and industrialization, the Earth's resources are being pushed to the brink of depletion. Non-sustainable industrial practices are not only endangering the supply of the Earth's natural resources, but are also putting burden on life itself by bringing about pollution and climate change. A major role of earth science scholars is to examine the delicate balance between the Earth's resources and the growing demands of industrialization. Through research and development, earth scientists have the power to preserve the planet's different resource domains by providing expert opinion and information about the forces which make life possible on Earth. We would like to express our sincere gratitude to all in the Technical Program Committee who have reviewed the papers and developed a very interesting Conference Program as well as the invited and plenary speakers. This year, we received 98 papers and after rigorous review, 17 papers were accepted. The participants come from eight countries. There are four Parallel Sessions and two invited Speakers. It is an honour to present this volume of IOP Conference Series: Earth and Environmental Science (EES) and we deeply thank the authors for their enthusiastic and high-grade contributions. Finally, we would like to thank the conference chairmen, the members of the steering committee, the organizing committee

  12. Smart rotor modeling aero-servo-elastic modeling of a smart rotor with adaptive trailing edge flaps

    CERN Document Server

    Bergami, Leonardo

    2014-01-01

    A smart rotor is a wind turbine rotor that, through a combination of sensors, control units and actuators actively reduces the variation of the aerodynamic loads it has to withstand. Smart rotors feature?promising load alleviation potential and might provide the technological breakthrough required by the next generation of large wind turbine rotors.The book presents the aero-servo-elastic model of a smart rotor with Adaptive Trailing Edge Flaps for active load alleviation and provides an insight on the rotor aerodynamic, structural and control modeling. A novel model for the unsteady aerodynam

  13. One Generation of New Material, One Generation of New Type Engine:Development Trend of Aero-engine and Its Requirements for Materials

    Directory of Open Access Journals (Sweden)

    LIU Da-xiang

    2017-10-01

    Full Text Available Based on the brief review of accelerated developing status of aircraft power technology in the world, the present status and developing trend of key materials technology for aero-engine were analyzed. In accordance with the idea of "one generation of new material, one generation of new type engine", development requirements for the materials technology of the system and main parts of aero-engine were proposed. Suggestions for improving development and application level of the materials technology in China were presented from aspects of quality stability and technical maturity, investigation and verification for engineering, materials system and data, composite materials, airworthiness certificate,etc.

  14. Modeling C-Band Co-Channel Interference From AeroMACS Omni-Directional Antennas to Mobile Satellite Service Feeder Uplinks

    Science.gov (United States)

    Wilson, Jeffrey D.

    2011-01-01

    A new C-band (5091 to 5150 MHz) airport communications system designated as Aeronautical Mobile Airport Communications System (AeroMACS) is being planned under the Federal Aviation Administration s NextGen program. An interference analysis software program, Visualyse Professional (Transfinite Systems Ltd), is being utilized to provide guidelines on limitations for AeroMACS transmitters to avoid interference with other systems. A scenario consisting of a single omni-directional transmitting antenna at each of the major contiguous United States airports is modeled and the steps required to build the model are reported. The results are shown to agree very well with a previous study.

  15. The AERO system: a 3D-like approach for recording gene expression patterns in the whole mouse embryo.

    Directory of Open Access Journals (Sweden)

    Hirohito Shimizu

    Full Text Available We have recently constructed a web-based database of gene expression in the mouse whole embryo, EMBRYS (http://embrys.jp/embrys/html/MainMenu.html. To allow examination of gene expression patterns to the fullest extent possible, this database provides both photo images and annotation data. However, since embryos develop via an intricate process of morphogenesis, it would be of great value to track embryonic gene expression from a three dimensional perspective. In fact, several methods have been developed to achieve this goal, but highly laborious procedures and specific operational skills are generally required. We utilized a novel microscopic technique that enables the easy capture of rotational, 3D-like images of the whole embryo. In this method, a rotary head equipped with two mirrors that are designed to obtain an image tilted at 45 degrees to the microscope stage captures serial images at 2-degree intervals. By a simple operation, 180 images are automatically collected. These 2D images obtained at multiple angles are then used to reconstruct 3D-like images, termed AERO images. By means of this system, over 800 AERO images of 191 gene expression patterns were captured. These images can be easily rotated on the computer screen using the EMBRYS database so that researchers can view an entire embryo by a virtual viewing on a computer screen in an unbiased or non-predetermined manner. The advantages afforded by this approach make it especially useful for generating data viewed in public databases.

  16. Polypyrrole/silver coaxial nanowire aero-sponges for temperature-independent stress sensing and stress-triggered Joule heating.

    Science.gov (United States)

    He, Weina; Li, Guangyong; Zhang, Shangquan; Wei, Yong; Wang, Jin; Li, Qingwen; Zhang, Xuetong

    2015-04-28

    To obtain ideal sensing materials with nearly zero temperature coefficient resistance (TCR) for self-temperature-compensated pressure sensors, we proposed an Incipient Network Conformal Growth (INCG) technology to prepare hybrid and elastic porous materials: the nanoparticles (NPs) are first dispersed in solvent to form an incipient network, another component is then introduced to coat the incipient network conformally via wet chemical route. The conformal coatings not only endow NPs with high stability but also offer them additional structural elasticity, meeting requirements for future generations of portable, compressive and flexible devices. The resultant polypyrrole/silver coaxial nanowire hybrid aero-sponges prepared via INCG technology have been processed into a piezoresistive sensor with highly sensing stability (low TCR 0.86 × 10(-3)/°C), sensitivity (0.33 kPa(-1)), short response time (1 ms), minimum detectable pressure (4.93 Pa) after suffering repeated stimuli, temperature change and electric heating. Moreover, a stress-triggered Joule heater can be also fabricated mainly by the PPy-Ag NW hybrid aero-sponges with nearly zero temperature coefficient.

  17. Emerging and established global life-style risk factors for cancer of the upper aero-digestive tract.

    Science.gov (United States)

    Gupta, Bhawna; Johnson, Newell W

    2014-01-01

    Upper aero-digestive tract cancer is a multidimensional problem, international trends showing complex rises and falls in incidence and mortality across the globe, with variation across different cultural and socio-economic groups. This paper seeks some explanations and identifies some research and policy needs. The literature illustrates the multifactorial nature of carcinogenesis. At the cellular level, it is viewed as a multistep process involving multiple mutations and selection for cells with progressively increasing capacity for proliferation, survival, invasion, and metastasis. Established and emerging risk factors, in addition to changes in incidence and prevalence of cancers of the upper aero-digestive tract, were identified. Exposure to tobacco and alcohol, as well as diets inadequate in fresh fruits and vegetables, remain the major risk factors, with persistent infection by particular so-called "high risk" genotypes of human papillomavirus increasingly recognised as also playing an important role in a subset of cases, particularly for the oropharynx. Chronic trauma to oral mucosa from poor restorations and prostheses, in addition to poor oral hygiene with a consequent heavy microbial load in the mouth, are also emerging as significant risk factors. Understanding and quantifying the impact of individual risk factors for these cancers is vital for health decision-making, planning and prevention. National policies and programmes should be designed and implemented to control exposure to environmental risks, by legislation if necessary, and to raise awareness so that people are provided with the information and support they need to adopt healthy lifestyles.

  18. Effective L/D: A Theoretical Approach to the Measurement of Aero-Structural Efficiency in Aircraft Design

    Science.gov (United States)

    Guynn, Mark D.

    2015-01-01

    There are many trade-offs in aircraft design that ultimately impact the overall performance and characteristics of the final design. One well recognized and well understood trade-off is that of wing weight and aerodynamic efficiency. Higher aerodynamic efficiency can be obtained by increasing wing span, usually at the expense of higher wing weight. The proper balance of these two competing factors depends on the objectives of the design. For example, aerodynamic efficiency is preeminent for sailplanes and long slender wings result. Although the wing weight-drag trade is universally recognized, aerodynamic efficiency and structural efficiency are not usually considered in combination. This paper discusses the concept of "aero-structural efficiency," which combines weight and drag characteristics. A metric to quantify aero-structural efficiency, termed effective L/D, is then derived and tested with various scenarios. Effective L/D is found to be a practical and robust means to simultaneously characterize aerodynamic and structural efficiency in the context of aircraft design. The primary value of the effective L/D metric is as a means to better communicate the combined system level impacts of drag and structural weight.

  19. Surface integrity of GH4169 affected by cantilever finish grinding and the application in aero-engine blades

    Directory of Open Access Journals (Sweden)

    Li Xun

    2015-10-01

    Full Text Available GH4169 is the main material for aero-engine blades and integrated blisks. Because GH4169 has a poor milling performance, the profile precision and surface integrity of blades and integrated blisks are difficult to be met by utilizing the conventional milling process, which directly influence the global performance and reliability of aero-engines. Through grinding experiments on parameters and surface integrity optimization, the helical cantilever grinding process utilizing a 300# CBN RB wheel is presented and applied in finish machining of GH4169 blades. The profile errors of the blade surface are within ±0.01 mm, the roughness is less than 0.4 μm, the residual compressive stresses and the hardening rate are appropriate, there are no phenomena of burr and smearing with the grinding chips, and the leading/trailing edge can be smoothly connected with the suction/pressure surface. All the experimental results indicate that this grinding process is greatly suitable for the profile finish machining of GH4169 blades.

  20. Nonlinear Dynamic Modeling of a Supersonic Commercial Transport Turbo-Machinery Propulsion System for Aero-Propulso-Servo-Elasticity Research

    Science.gov (United States)

    Connolly, Joe; Carlson, Jan-Renee; Kopasakis, George; Woolwine, Kyle

    2015-01-01

    This paper covers the development of an integrated nonlinear dynamic model for a variable cycle turbofan engine, supersonic inlet, and convergent-divergent nozzle that can be integrated with an aeroelastic vehicle model to create an overall Aero-Propulso-Servo-Elastic (APSE) modeling tool. The primary focus of this study is to provide a means to capture relevant thrust dynamics of a full supersonic propulsion system by using relatively simple quasi-one dimensional computational fluid dynamics (CFD) methods that will allow for accurate control algorithm development and capture the key aspects of the thrust to feed into an APSE model. Previously, propulsion system component models have been developed and are used for this study of the fully integrated propulsion system. An overview of the methodology is presented for the modeling of each propulsion component, with a focus on its associated coupling for the overall model. To conduct APSE studies the described dynamic propulsion system model is integrated into a high fidelity CFD model of the full vehicle capable of conducting aero-elastic studies. Dynamic thrust analysis for the quasi-one dimensional dynamic propulsion system model is presented along with an initial three dimensional flow field model of the engine integrated into a supersonic commercial transport.

  1. N3S-AERO: a multidimensional model for numerical simulation of all wet cooling tower systems

    International Nuclear Information System (INIS)

    Razafindrakoto, E.; Hofmann, F.

    1997-01-01

    3D model is more required to optimize the design of new cooling tower by way of parameters studies, to improve the performance of the existing ones from changes in fill zone or water distribution. Therefore, the Directions des Etudes et Recherches with collaboration of the Direction de l'Equipement of EDF, has developed a specific version of the finite element CFD code N3S, denoted N3S-AERO, for the simulation of natural or mechanical draught wet cooling towers. It solves mass, momentum, heat and humidity averaged Navier-Stokes equations including buoyancy terms with variable density for air flow in the whole domain mass, heat equations for water flow in exchange zones. With standard results of N3S as air velocity and scalar fields, N3S-AERO gives in return water temperature fields mean values of variables at inlet or outlet of each exchange zone and thermal performance of the tower. 2D axisymmetrical and 3D industrial cases have soon been done. Major flow phenomena are well predicted and averaged cold water values are in good agreement with ID-TEFERI code or measurements

  2. Rare earth oxide aero- and xerogels. Tuning porosity and catalytic properties

    Energy Technology Data Exchange (ETDEWEB)

    Neumann, Bjoern

    2013-11-15

    , katalytisch vielversprechende Seltenerdoxide im Hinblick auf Porositaet und Zusammensetzung so zu veraendern, dass sie fuer Oxidationsreaktionen und die oxidative Kupplung von Methan gute Ergebnisse aufweisen. Dabei lag einerseits ein grosser Schwerpunkt auf Sol-gel-chemischen Methoden und hier besonders auf der sog. ''Epoxide Addition Method''. Neben Aero- und Xerogelen der reinen Seltenerdoxide wurden auch Hybridsysteme aus den Seltenerdoxiden und Aluminiumoxid praepariert, umfangreich charakterisiert und katalytisch getestet. Des Weiteren wurden duenne Xerogel Filme und makroporoese Monolithe, letztere mittels einer direkten Schaeumungsmethode, hergestellt. Die Ergebnisse der Arbeit belegen das grosse Potential v.a. der Sol-Gel-Chemie, poroese Materialien mit variabler und kontrollierbarer Porositaet und Zusammensetzung fuer die heterogene Katalyse verfuegbar zu machen und dabei leistungsfaehigere Katalysatoren zu erhalten.

  3. Investigation of global particulate nitrate from the AeroCom phase III experiment

    Directory of Open Access Journals (Sweden)

    H. Bian

    2017-11-01

    Full Text Available An assessment of global particulate nitrate and ammonium aerosol based on simulations from nine models participating in the Aerosol Comparisons between Observations and Models (AeroCom phase III study is presented. A budget analysis was conducted to understand the typical magnitude, distribution, and diversity of the aerosols and their precursors among the models. To gain confidence regarding model performance, the model results were evaluated with various observations globally, including ground station measurements over North America, Europe, and east Asia for tracer concentrations and dry and wet depositions, as well as with aircraft measurements in the Northern Hemisphere mid-to-high latitudes for tracer vertical distributions. Given the unique chemical and physical features of the nitrate occurrence, we further investigated the similarity and differentiation among the models by examining (1 the pH-dependent NH3 wet deposition; (2 the nitrate formation via heterogeneous chemistry on the surface of dust and sea salt particles or thermodynamic equilibrium calculation including dust and sea salt ions; and (3 the nitrate coarse-mode fraction (i.e., coarse/total. It is found that HNO3, which is simulated explicitly based on full O3-HOx-NOx-aerosol chemistry by all models, differs by up to a factor of 9 among the models in its global tropospheric burden. This partially contributes to a large difference in NO3−, whose atmospheric burden differs by up to a factor of 13. The atmospheric burdens of NH3 and NH4+ differ by 17 and 4, respectively. Analyses at the process level show that the large diversity in atmospheric burdens of NO3−, NH3, and NH4+ is also related to deposition processes. Wet deposition seems to be the dominant process in determining the diversity in NH3 and NH4+ lifetimes. It is critical to correctly account for contributions of heterogeneous chemical production of nitrate on dust and sea salt, because this process

  4. APPLICATION OF ROUGH SET THEORY TO MAINTENANCE LEVEL DECISION-MAKING FOR AERO-ENGINE MODULES BASED ON INCREMENTAL KNOWLEDGE LEARNING

    Institute of Scientific and Technical Information of China (English)

    陆晓华; 左洪福; 蔡景

    2013-01-01

    The maintenance of an aero-engine usually includes three levels ,and the maintenance cost and period greatly differ depending on the different maintenance levels .To plan a reasonable maintenance budget program , airlines would like to predict the maintenance level of aero-engine before repairing in terms of performance parame-ters ,which can provide more economic benefits .The maintenance level decision rules are mined using the histori-cal maintenance data of a civil aero-engine based on the rough set theory ,and a variety of possible models of upda-ting rules produced by newly increased maintenance cases added to the historical maintenance case database are in-vestigated by the means of incremental machine learning .The continuously updated rules can provide reasonable guidance suggestions for engineers and decision support for planning a maintenance budget program before repai-ring .The results of an example show that the decision rules become more typical and robust ,and they are more accurate to predict the maintenance level of an aero-engine module as the maintenance data increase ,which illus-trates the feasibility of the represented method .

  5. On the aero-elastic design of the DTU 10MW wind turbine blade for the LIFES50+ wind tunnel scale model

    DEFF Research Database (Denmark)

    Bayati, I.; Belloli, M.; Bernini, L.

    2016-01-01

    and for different angles of attack. The aero-elastic design algorithm was set to define the optimal spanwise thickness over chord ratio (t/c), the chord length and the twist to match the first flapwise scaled natural frequency. An aluminium mould for the carbon fibre was CNC manufactured based on B-Splines CAD...

  6. Evaluation of cardiac adrenergic neuronal damage in rats with doxorubicin-induced cardiomyopathy using iodine-131 MIBG autoradiography and PGP 9.5 immunohistochemistry

    International Nuclear Information System (INIS)

    Jeon, T.J.; Lee, J.D.; Ha, J.-W.; Yang, W.I.; Cho, S.H.

    2000-01-01

    Doxorubicin is one of the most useful anticancer agents, but its repeated administration can induce irreversible cardiomyopathy as a major complication. The purpose of this study was to investigate doxorubicin toxicity on cardiac sympathetic neurons using iodine-131-metaiodobenzylguanidine (MIBG) and protein gene product (PGP) 9.5 immunohistochemistry, which is a marker of cardiac innervation. Wistar rats were treated with doxorubicin (2 mg/kg, i.v.) once a week for 4 (n=5), 6 (n=6) or 8 (n=7) weeks consecutively. Left ventricular ejection fraction (LVEF), calculated by M-mode echocardiography, was used as an indicator of cardiac function. Plasma noradrenaline (NA) concentration was measured by high-performance liquid chromatography (HPLC). 131 I-MIBG uptake of the left ventricular wall (24 ROIs) was measured by autoradiography. 131 I-MIBG uptake pattern was compared with histopathological results, the neuronal population on PGP 9.5 immunohistochemistry and the degree of myocyte damage assessed using a visual scoring system on haematoxylin and eosin and Masson's trichrome staining. LVEF was significantly decreased in the 8-week group (P 131 I-MIBG uptake ratio of subepicardium to subendocardium were significantly increased (P<0.05) in the 8-week group as compared with the control group. It may be concluded that radioiodinated MIBG is a reliable marker for the detection of cardiac adrenergic neuronal damage in doxorubicin-induced cardiomyopathy; it detects such damage earlier than do other clinical parameters and in this study showed a good correlation with the reduction in the neuronal population on PGP 9.5 stain. The subendocardial layer appeared to be more vulnerable to doxorubicin than the subepicardium. (orig.)

  7. Long wavelength stimulated emission up to 9.5 μm from HgCdTe quantum well heterostructures

    Energy Technology Data Exchange (ETDEWEB)

    Morozov, S. V.; Rumyantsev, V. V., E-mail: rumyantsev@ipmras.ru; Dubinov, A. A.; Kudryavtsev, K. E.; Antonov, A. V.; Gavrilenko, V. I. [Institute for Physics of Microstructures of Russian Academy of Sciences, 603950 Nizhny Novgorod (Russian Federation); Lobachevsky State University of Nizhny Novgorod, 603950 Nizhny Novgorod (Russian Federation); Kadykov, A. M. [Institute for Physics of Microstructures of Russian Academy of Sciences, 603950 Nizhny Novgorod (Russian Federation); UMR CNRS 5221, GIS-TERALAB, Université Montpellier II, 34095 Montpellier (France); Mikhailov, N. N. [A.V. Rzhanov Institute of Semiconductor Physics, Siberian Branch of Russian Academy of Sciences, 630090 Novosibirsk (Russian Federation); Novosibirsk State University, 630090 Novosibirsk (Russian Federation); Dvoretskii, S. A. [A.V. Rzhanov Institute of Semiconductor Physics, Siberian Branch of Russian Academy of Sciences, 630090 Novosibirsk (Russian Federation)

    2016-02-29

    Stimulated emission from waveguide HgCdTe structures with several quantum wells inside waveguide core is demonstrated at wavelengths up to 9.5 μm. Photoluminescence line narrowing down to kT energy, as well as superlinear rise in its intensity evidence the onset of the stimulated emission, which takes place under optical pumping with intensity as small as ∼0.1 kW/cm{sup 2} at 18 K and 1 kW/cm{sup 2} at 80 K. One can conclude that HgCdTe structures potential for long-wavelength lasers is not exhausted.

  8. Host model uncertainties in aerosol radiative forcing estimates: results from the AeroCom Prescribed intercomparison study

    Directory of Open Access Journals (Sweden)

    P. Stier

    2013-03-01

    Full Text Available Simulated multi-model "diversity" in aerosol direct radiative forcing estimates is often perceived as a measure of aerosol uncertainty. However, current models used for aerosol radiative forcing calculations vary considerably in model components relevant for forcing calculations and the associated "host-model uncertainties" are generally convoluted with the actual aerosol uncertainty. In this AeroCom Prescribed intercomparison study we systematically isolate and quantify host model uncertainties on aerosol forcing experiments through prescription of identical aerosol radiative properties in twelve participating models. Even with prescribed aerosol radiative properties, simulated clear-sky and all-sky aerosol radiative forcings show significant diversity. For a purely scattering case with globally constant optical depth of 0.2, the global-mean all-sky top-of-atmosphere radiative forcing is −4.47 Wm−2 and the inter-model standard deviation is 0.55 Wm−2, corresponding to a relative standard deviation of 12%. For a case with partially absorbing aerosol with an aerosol optical depth of 0.2 and single scattering albedo of 0.8, the forcing changes to 1.04 Wm−2, and the standard deviation increases to 1.01 W−2, corresponding to a significant relative standard deviation of 97%. However, the top-of-atmosphere forcing variability owing to absorption (subtracting the scattering case from the case with scattering and absorption is low, with absolute (relative standard deviations of 0.45 Wm−2 (8% clear-sky and 0.62 Wm−2 (11% all-sky. Scaling the forcing standard deviation for a purely scattering case to match the sulfate radiative forcing in the AeroCom Direct Effect experiment demonstrates that host model uncertainties could explain about 36% of the overall sulfate forcing diversity of 0.11 Wm−2 in the AeroCom Direct Radiative Effect experiment. Host model errors in aerosol radiative forcing are largest in regions of uncertain host model

  9. 3D quantitative interpretation of archaeo-magnetic data: Adaptation of aero-magnetic interpretation techniques for archaeological purposes

    Science.gov (United States)

    Cheyney, S.; Hill, I. A.; Linford, N.; Fishwick, S.; Leech, C.

    2011-12-01

    High-resolution total-field magnetic data can be collected rapidly and relatively cheaply over large archaeological sites due to recent advances in data collection. However, interpretation of these datasets still generally comprises a sequence of data correction and filtering operations prior to a 2D visual interpretation based on pattern recognition. In contrast, current developments in aero-magnetic interpretation have led to several tools for identifying location, shape and depth information of anomalous sources. These methods often fail when directly applied to archaeo-magnetic data, due to the particular noise content typical in very near-surface surveys. Here techniques are explored that allow these aero-magnetic interpretation tools to be applied to archaeological problems, without the need for extensive, often biased user input. It is shown that full 3D quantitative interpretation of the subsurface is possible from just the magnetic data alone. Inversion of magnetic data is increasingly being applied to aero-magnetic surveys to produce 3D models of the subsurface magnetisation. Typically, an objective function is minimised in order to create a smooth distribution of magnetisation away from a reference model (or halfspace if no a-priori information is available). Often, although a good fit to the observed values may be obtained, the final model will be non-unique and biased by the reference model. Testing of synthetic data shows that when archaeo-magnetic datasets are inverted without applying a-priori information, large discrepancies between the true and modelled depths can occur. Where no a-priori information is available, information regarding the horizontal location of sources can be obtained from derivative-based methods such as the absolute horizontal gradient, tilt-angle and theta-map. Using pseudogravity data with these techniques, overcomes the problem of noise amplification that has previously hampered archaeological uses of these techniques. Depth

  10. Aero-Propulsive Model Design from a Commercial Aircraft in Climb and Cruise Regime using Performance Data =

    Science.gov (United States)

    Tudor, Magdalena

    IATA has estimated, in 2012, at about 2% of global carbon dioxide emissions, the environmental impact of the air transport, as a consequence caused by the rapidly growing of global movement demand of people and goods, and which was effectively taken into account in the development of the aviation industry. The historic achievements of scientific and technical progress in the field of commercial aviation were contributed to this estimate, and even today the research continues to make progress to help to reduce the emissions of greenhouse gases. Advances in commercial aircraft, and its engine design technology had the aim to improve flight performance. These improvements have enhanced the global flight planning of these types of aircrafts. Almost all of these advances rely on generated performance data as reference sources, the most of which are classified as "confidential" by the aircraft manufacturers. There are very few aero-propulsive models conceived for the climb regime in the literature, but none of them was designed without access to an engine database, and/or to performance data in climb and in cruise regimes with direct applicability for flight optimization. In this thesis, aero-propulsive models methodologies are proposed for climb and cruise regimes, using system identification and validation methods, through which airplane performance can be computed and stored in the most compact and easily accessible format for this kind of performance data. The acquiring of performance data in this format makes it possible to optimize flight profiles, used by on-board Flight Management Systems. The aero-propulsive models developed here were investigated on two aircrafts belonging to commercial class, and both of them had offered very good accuracy. One of their advantages is that they can be adapted to any other aircraft of the same class, even if there is no access to their corresponding engine flight data. In addition, these models could save airlines a considerable

  11. HAWC2 and BeamDyn: Comparison Between Beam Structural Models for Aero-Servo-Elastic Frameworks: Preprint

    Energy Technology Data Exchange (ETDEWEB)

    Pavese, Christian; Kim, Taeseong; Wang, Qi; Jonkman, Jason; Sprague, Michael A.

    2016-08-01

    This work presents a comparison of two beam codes for aero-servo-elastic frameworks: a new structural model for the aeroelastic code HAWC2 and a new nonlinear beam model, BeamDyn, for the aeroelastic modularization framework FAST v8. The main goal is to establish the suitability of the two approaches to model the structural behaviour of modern wind turbine blades in operation. Through a series of benchmarking structural cases of increasing complexity, the capability of the two codes to simulate highly nonlinear effects is investigated and analyzed. Results show that even though the geometrically exact beam theory can better model effects such as very large deflections, rotations, and structural couplings, an approach based on a multi-body formulation assembled through linear elements is capable of computing accurate solutions for typical nonlinear beam theory benchmarking cases.

  12. Initial comments on the aero geophysical information present at the B and C areas of the Itatira (Brazil) project

    International Nuclear Information System (INIS)

    Castro, Neivaldo Araujo de; Castelo Branco, Raimundo Mariano Gomes

    1999-01-01

    The aero geophysical project called Itatira,, accomplished by LASA Engenharia e Prospeccoes S.A., Between September and November/1977 through contract with NUCLEBRAS, corresponds to one of the first project of this gender accomplished in national territory. In this project were flight more than 80 000 km of linear lines, which covered approximately 38 000 km 2 on the precambrian terrains of the Ceara State, NE Brazil. For several reasons, the total area of the project was subdivided in three sub-areas (A, B and C), each one covered by a different airship (LAS, 1977). This paper presents the geophysical information and preliminary interpretations of the areas B and C that were obtained through the integrated use of the soft wares AUTOCAD r. 14, OASIS MONTAJ r.4.2 and ERMAPPER r.5.5. (author)

  13. Expansion of plasma of electrically exploding single copper wire under 4.5 kA-9.5 kA/wire

    International Nuclear Information System (INIS)

    Li Yexun; Yang Libing; Sun Chengwei

    2003-01-01

    The experimental system for electrically exploding single metal wire has been designed and manufactured. Expansion of the dense plasma column formed from an electrically exploding Cu wire of diameter 30 μm has been studied with a high-speed photographer to obtain the time-dependent radius (R-t) curve. The experimental results demonstrate that the mean expansion rate of the dense plasma column is 1.94 μm/ns, 2.6 μm/ns and 3.75 μm/ns according to the peak pulse current 4.5 kA, 7 kA and 9.5 kA respectively. The results can be beneficial to giving a profound understanding of the early stage of wire-array Z-pinch physics and to improvement on their design

  14. Acrania/encephalocele sequence (exencephaly) associated with 92,XXXX karyotype: early prenatal diagnosis at 9(+5) weeks by 3D transvaginal ultrasound and coelocentesis.

    Science.gov (United States)

    Tonni, Gabriele; Ventura, Alessandro; Bonasoni, Maria Paola

    2009-09-01

    A 27-year-old pregnant woman was diagnosed by 3D transvaginal ultrasound as carrying a fetus of 9(+5) weeks gestation affected by acrania/encephalocele (exencephaly) sequence. A 2D transvaginal ultrasound-guided aspiration of 5 mL of extra-coelomic fluid was performed under cervical block before uterine suction. Conventional cytogenetic analysis demonstrated a 92,XXXX karyotype. Transvaginal 2D ultrasound-guided coelocentesis for rapid karyotyping can be proposed to women who are near to miscarriage or in cases where a prenatal ultrasound diagnosis of congenital anomaly is performed at an early stage of development. Genetic analysis can be performed using traditional cytogenetic analysis or can be aided by fluorescence in situ hybridization (FISH). Coelocentesis may become an integral part of first trimester armamentarium and may be clinically useful in the understanding of the pathogenesis of early prenatally diagnosed congenital anomalies.

  15. 78 FR 49982 - Airworthiness Directives; Saab AB, Saab Aerosystems Airplanes

    Science.gov (United States)

    2013-08-16

    ... ducts to gain access to the drive motor. (4) Disconnect power leads from motor terminals (1/4-28). Tag... verify proper operation. Therefore, connect ground power source or verify aircraft power is on and turn...) Disconnect power leads from motor terminals (1/4-28). Tag positive lead. (iv) Remove condenser support...

  16. 77 FR 29855 - Airworthiness Directives; Saab AB, Saab Aerosystems Airplanes

    Science.gov (United States)

    2012-05-21

    ... electronic installation wiring. For the reasons described above, this [EASA] AD requires a one- time... corrosion of the electrical and electronics installation, and if corrosion is found repairing each affected harness braid or replacing each affected component and/or wiring harness. We are issuing this AD to detect...

  17. 77 FR 11791 - Airworthiness Directives; Saab AB, Saab Aerosystems Airplanes

    Science.gov (United States)

    2012-02-28

    ... installation wiring. For the reasons described above, this [EASA] AD requires a one- time [detailed] inspection... installation, and if corrosion is found repairing each affected harness braid or replacing each affected component and/or wiring harness. We are proposing this AD to detect and correct corrosion of critical system...

  18. Re-irradiation associated to cetuximab and paclitaxel in the recurrences in irradiated field of upper aero-digestive ducts tumors resistant to platina salts; Re-irradiation associee au cetuximab et au paclitaxel dans les recidives en territoire irradie des tumeurs des voies aero-digestives superieures resistantes aux sels de platine

    Energy Technology Data Exchange (ETDEWEB)

    Martin, L.M. [Centre Guillaume-Le-Conquerant, 76 - Le Havre (France); Moran, A.R.; Pavlovitch, J.M. [Clinique du Petit-Colmoulin, 76 - Harfleur (France); El Amarti, R. [Hopital Monod, 76 - Montivilliers (France); Damour, M. [CMC Ormeaux-Vauban, 76 - Le Havre (France)

    2007-11-15

    The objective of this study is to present the preliminary results of the toxicity and efficiency evaluation of the association 're-irradiation-cetuximab-paclitaxel' in the recurrences of upper aero-digestive ducts tumors in irradiated field resistant to platinum salts. (N.C.)

  19. Electron-beam-welded segmental heat pipes of AlMgSi 1 for the thermal model of the satellite Aeros-A

    Energy Technology Data Exchange (ETDEWEB)

    Hoell, H.; Lasar, H.

    1974-07-01

    For the purposes of tests with the thermal model of the German aeronomy satellite Aeros-A, a heat pipe system of optimized weight was developed in order to transport thermal energy from the solar cells of the cylindrical satellite to the conical bottom. Because of stringent requirements on the fabrication process, electron beam welding is used for bonding. The welding process is described and preliminary test results are given. (LEW)

  20. THE APPLICATION OF REMOTE SENSING AND AERO-GEOPHYSICS DATA FUSION ON METALLOGENIC PROGNOSIS IN QIMANTAGE OF EAST KUNLUN MONTAIN AREA

    OpenAIRE

    Jia, W.; Zhang, H.; Lin, J.; Zhao, H.

    2013-01-01

    Based on west of Qimantage of East Kunlun mountain area, takes advantage of ASTER data, according to the altered mineral spectral characteristics, remote sensing alteration information is extracted. Incorporation the anomaly extraction results with high-precision aero geophysical data processing results, a multiple resource information fusion model is proposed. The fusion model of two totally different type of data which is a special attention in geospatial academia now, which can im...

  1. Simulating Global AeroMACS Airport Ground Station Antenna Power Transmission Limits to Avoid Interference With Mobile Satellite Service Feeder Uplinks

    Science.gov (United States)

    Wilson, Jeffrey D.

    2013-01-01

    The Aeronautical Mobile Airport Communications System (AeroMACS), which is based upon the IEEE 802.16e mobile wireless standard, is expected to be implemented in the 5091 to 5150 MHz frequency band. As this band is also occupied by Mobile Satellite Service feeder uplinks, AeroMACS must be designed to avoid interference with this incumbent service. The aspects of AeroMACS operation that present potential interference are under analysis in order to enable the definition of standards that assure that such interference will be avoided. In this study, the cumulative interference power distribution at low Earth orbit from transmitters at global airports was simulated with the Visualyse Professional software. The dependence of the interference power on antenna distribution, gain patterns, duty cycle, and antenna tilt was simulated. As a function of these parameters, the simulation results are presented in terms of the limitations on transmitter power from global airports required to maintain the cumulative interference power under the established threshold.

  2. A TALE OF DWARFS AND GIANTS: USING A z = 1.62 CLUSTER TO UNDERSTAND HOW THE RED SEQUENCE GREW OVER THE LAST 9.5 BILLION YEARS

    International Nuclear Information System (INIS)

    Rudnick, Gregory H.; Tran, Kim-Vy; Papovich, Casey; Momcheva, Ivelina; Willmer, Christopher

    2012-01-01

    We study the red sequence in a cluster of galaxies at z = 1.62 and follow its evolution over the intervening 9.5 Gyr to the present day. Using deep YJK s imaging with the HAWK-I instrument on the Very Large Telescope, we identify a tight red sequence and construct its rest-frame i-band luminosity function (LF). There is a marked deficit of faint red galaxies in the cluster that causes a turnover in the LF. We compare the red-sequence LF to that for clusters at z 0.6. In this model the cluster accretes blue galaxies from the field whose star formation is quenched and who are subsequently allowed to merge. We find that three to four mergers among cluster galaxies during the 4 Gyr between z = 1.62 and z = 0.6 match the observed LF evolution between the two redshifts. The inferred merger rate is consistent with other studies of this cluster. Our result supports the picture that galaxy merging during the major growth phase of massive clusters is an important process in shaping the red-sequence population at all luminosities.

  3. Thermally assisted interlayer magnetic coupling through Ba_0_._0_5Sr_0_._9_5TiO_3 barriers

    International Nuclear Information System (INIS)

    Carreira, Santiago J.; Steren, Laura B.; Avilés Félix, Luis; Alejandro, Gabriela; Sirena, Martín

    2016-01-01

    We report on the interlayer exchange coupling across insulating barriers observed on Ni_8_0Fe_2_0/Ba_0_._0_5Sr_0_._9_5TiO_3/La_0_._6_6Sr_0_._3_3MnO_3 (Py/BST_0_._0_5/LSMO) trilayers. The coupling mechanism has been analyzed in terms of the barrier thickness, samples' substrate, and temperature. We examined the effect of MgO (MGO) and SrTiO_3 (STO) (001) single-crystalline substrates on the magnetic coupling and also on the magnetic anisotropies of the samples in order to get a deeper understanding of the magnetism of the structures. We measured a weak coupling mediated by spin-dependent tunneling phenomena whose sign and strength depend on barrier thickness and substrate. An antiferromagnetic (AF) exchange prevails for most of the samples and smoothly increases with the barrier thicknesses as a consequence of the screening effects of the BST_0_._0_5. The coupling monotonically increases with temperature in all the samples and this behavior is attributed to thermally assisted mechanisms. The magnetic anisotropy of both magnetic components has a cubic symmetry that in the case of permalloy is added to a small uniaxial component.

  4. Effect of TiC additions to the microstructure and magnetic properties of Nd9.5Fe84.5B6 melt-spun ribbons

    International Nuclear Information System (INIS)

    Kramer, M.J.; Li, C.P.; Dennis, K.W.; McCallum, R.W.; Sellers, C.H.; Branagan, D.J.; Lewis, L.H.; Wang, J.Y.

    1998-01-01

    Rapidly solidified samples of Nd 9.5 Fe 84.5 B 6 with and without 3 at.% TiC were prepared by melt spinning and melt extraction and then annealed in vacuum (3x10 -6 Torr) at temperatures from 600 to 750 degree C. For alloys melt spun under similar conditions, the overquenched state was achieved at wheel speeds >10 m/s for the TiC added alloy while >20 m/s was necessary without TiC. The overquenched samples contained a smaller fraction of α-Fe in smaller grains than the undercooled samples where Fe dendrites formed near the free surface during solidification. These Fe dendrites were not removed by annealing. In addition, large orientated 2-14-1 grains nucleated on the Fe dendrites. This combination is detrimental to the magnetic properties. The addition of TiC results in improved control of the microstructure over a larger fraction of the ribbon volume enhancing the magnetic properties. copyright 1998 American Institute of Physics

  5. Muusika saab rõivasteks

    Index Scriptorium Estoniae

    2003-01-01

    Itaalia professori Fabio Sartorelli teaduseksperimendist tõlkida muusikalised noodid ja rütmid mustrite, triipude ja värvide keelde ja kanda need kangale. Itaalia firma Paul & Shark rõivakollektsioonist "Kanna muusikat, mis sulle meeldib"

  6. Unistus saab reaalsuseks / Kadri Kaldam

    Index Scriptorium Estoniae

    Kaldam, Kadri

    2008-01-01

    Arhitektuuri ja disaini veebiportaali Architonic salong Kölni mööblimessil. Projekteerija: LAVA (Laboratory for Visionary Architecture, Stuttgart, Sydney). Arhitektid: Tobias Wallisser, Chris Bosse. Loov meeskond: Kadri Kaldam, Stephan M. Albrecht, Kristof Gavrielides

  7. The Chiloé Mw 7.6 earthquake of 2016 December 25 in Southern Chile and its relation to the Mw 9.5 1960 Valdivia earthquake

    Science.gov (United States)

    Lange, Dietrich; Ruiz, Javier; Carrasco, Sebastián; Manríquez, Paula

    2018-04-01

    On 2016 December 25, an Mw 7.6 earthquake broke a portion of the Southern Chilean subduction zone south of Chiloé Island, located in the central part of the Mw 9.5 1960 Valdivia earthquake. This region is characterized by repeated earthquakes in 1960 and historical times with very sparse interseismic activity due to the subduction of a young (˜15 Ma), and therefore hot, oceanic plate. We estimate the coseismic slip distribution based on a kinematic finite-fault source model, and through joint inversion of teleseismic body waves and strong motion data. The coseismic slip model yields a total seismic moment of 3.94 × 1020 N.m that occurred over ˜30 s, with the rupture propagating mainly downdip, reaching a peak slip of ˜4.2 m. Regional moment tensor inversion of stronger aftershocks reveals thrust type faulting at depths of the plate interface. The fore- and aftershock seismicity is mostly related to the subduction interface with sparse seismicity in the overriding crust. The 2016 Chiloé event broke a region with increased locking and most likely broke an asperity of the 1960 earthquake. The updip limit of the main event, aftershocks, foreshocks and interseismic activity are spatially similar, located ˜15 km offshore and parallel to Chiloé Islands west coast. The coseismic slip model of the 2016 Chiloé earthquake suggests a peak slip of 4.2 m that locally exceeds the 3.38 m slip deficit that has accumulated since 1960. Therefore, the 2016 Chiloé earthquake possibly released strain that has built up prior to the 1960 Valdivia earthquake.

  8. 76 FR 53301 - Airworthiness Directives; Saab AB, Saab Aerosystems Model SAAB 2000 Airplanes

    Science.gov (United States)

    2011-08-26

    ... pressure bulkhead, possibly resulting in in-flight decompression of the fuselage and injury to occupants... 44 U.S.C. 1510. #0; #0;The Code of Federal Regulations is sold by the Superintendent of Documents. #0... information (MCAI) originated by an aviation authority of another country to identify and correct an unsafe...

  9. Aero-thermal optimization of film cooling flow parameters on the suction surface of a high pressure turbine blade

    Science.gov (United States)

    El Ayoubi, Carole; Hassan, Ibrahim; Ghaly, Wahid

    2012-11-01

    This paper aims to optimize film coolant flow parameters on the suction surface of a high-pressure gas turbine blade in order to obtain an optimum compromise between a superior cooling performance and a minimum aerodynamic penalty. An optimization algorithm coupled with three-dimensional Reynolds-averaged Navier Stokes analysis is used to determine the optimum film cooling configuration. The VKI blade with two staggered rows of axially oriented, conically flared, film cooling holes on its suction surface is considered. Two design variables are selected; the coolant to mainstream temperature ratio and total pressure ratio. The optimization objective consists of maximizing the spatially averaged film cooling effectiveness and minimizing the aerodynamic penalty produced by film cooling. The effect of varying the coolant flow parameters on the film cooling effectiveness and the aerodynamic loss is analyzed using an optimization method and three dimensional steady CFD simulations. The optimization process consists of a genetic algorithm and a response surface approximation of the artificial neural network type to provide low-fidelity predictions of the objective function. The CFD simulations are performed using the commercial software CFX. The numerical predictions of the aero-thermal performance is validated against a well-established experimental database.

  10. Aerosol Vacuum-Assisted Plasma Ionization (Aero-VaPI) Coupled to Ion Mobility-Mass Spectrometry

    Science.gov (United States)

    Blair, Sandra L.; Ng, Nga L.; Zambrzycki, Stephen C.; Li, Anyin; Fernández, Facundo M.

    2018-02-01

    In this communication, we report on the real-time analysis of organic aerosol particles by Vacuum-assisted Plasma Ionization-Mass Spectrometry (Aero-VaPI-MS) using a home-built VaPI ion source coupled to a Synapt G2-S HDMS ion mobility-mass spectrometry (IM-MS) system. Standards of organic molecules of interest in prebiotic chemistry were used to generate aerosols. Monocaprin and decanoic acid aerosol particles were successfully detected in both the positive and negative ion modes, respectively. A complex aerosol mixture of different sizes of polymers of L-malic acid was also examined through ion mobility (IM) separations, resulting in the detection of polymers of up to eight monomeric units. This noncommercial plasma ion source is proposed as a low cost alternative to other plasma ionization platforms used for aerosol analysis, and a higher-performance alternative to more traditional aerosol mass spectrometers. VaPI provides robust online ionization of organics in aerosols without extensive ion activation, with the coupling to IM-MS providing higher peak capacity and excellent mass accuracy. [Figure not available: see fulltext.

  11. The effect of harmonized emissions on aerosol properties in global models – an AeroCom experiment

    Directory of Open Access Journals (Sweden)

    C. Textor

    2007-08-01

    Full Text Available The effects of unified aerosol sources on global aerosol fields simulated by different models are examined in this paper. We compare results from two AeroCom experiments, one with different (ExpA and one with unified emissions, injection heights, and particle sizes at the source (ExpB. Surprisingly, harmonization of aerosol sources has only a small impact on the simulated inter-model diversity of the global aerosol burden, and consequently global optical properties, as the results are largely controlled by model-specific transport, removal, chemistry (leading to the formation of secondary aerosols and parameterizations of aerosol microphysics (e.g., the split between deposition pathways and to a lesser extent by the spatial and temporal distributions of the (precursor emissions.

    The burdens of black carbon and especially sea salt become more coherent in ExpB only, because the large ExpA diversities for these two species were caused by a few outliers. The experiment also showed that despite prescribing emission fluxes and size distributions, ambiguities in the implementation in individual models can lead to substantial differences.

    These results indicate the need for a better understanding of aerosol life cycles at process level (including spatial dispersal and interaction with meteorological parameters in order to obtain more reliable results from global aerosol simulations. This is particularly important as such model results are used to assess the consequences of specific air pollution abatement strategies.

  12. A Mission Concept: Re-Entry Hopper-Aero-Space-Craft System on-Mars (REARM-Mars)

    Science.gov (United States)

    Davoodi, Faranak

    2013-01-01

    Future missions to Mars that would need a sophisticated lander, hopper, or rover could benefit from the REARM Architecture. The mission concept REARM Architecture is designed to provide unprecedented capabilities for future Mars exploration missions, including human exploration and possible sample-return missions, as a reusable lander, ascend/descend vehicle, refuelable hopper, multiple-location sample-return collector, laboratory, and a cargo system for assets and humans. These could all be possible by adding just a single customized Re-Entry-Hopper-Aero-Space-Craft System, called REARM-spacecraft, and a docking station at the Martian orbit, called REARM-dock. REARM could dramatically decrease the time and the expense required to launch new exploratory missions on Mars by making them less dependent on Earth and by reusing the assets already designed, built, and sent to Mars. REARM would introduce a new class of Mars exploration missions, which could explore much larger expanses of Mars in a much faster fashion and with much more sophisticated lab instruments. The proposed REARM architecture consists of the following subsystems: REARM-dock, REARM-spacecraft, sky-crane, secure-attached-compartment, sample-return container, agile rover, scalable orbital lab, and on-the-road robotic handymen.

  13. Elastic and inelastic scattering of 9,11 Li + Si at backward angles in the energy range (9.5 - 25) AMeV

    International Nuclear Information System (INIS)

    Petrascu, M.; Bordeanu, C.; Isbasescu, A.; Mihai, I.; Giurgiu, M.

    1997-01-01

    Recently, an inclusive fusion experiment of 9,11 Li projectiles with Si targets, in the energy range (9.5 - 25) AMeV has been performed at Riken Ring Cyclotron-Japan using, for the detection of the fusion products, an ionization chamber, MUSIC, built in NIPNE-HH, Bucharest. In this experiment, the contribution of elastic and inelastic scattering, at forward detection angles is eliminated through the experimental set-up. For a clear investigation of the fusion process, the estimation of elastic and inelastic scattering at backward angles, between 80 angle - 180 angle was considered necessary. This estimation was made by the coupled channels computer code ECIS. ECIS is an iterative method, the first iteration of this procedure being DWBA. In the analysis of elastic and inelastic scattering of 9,11 Li projectile on Si target we assumed that the incident 9 Li and 11 Li waves are diffracted by an optical potential with an Woods-Saxon geometry. The adopted optical potential is given. For the depth of the real and imaginary volume terms we used values dependent on projectile energy and target mass number. These values have been chosen in good agreement with a semi-microscopic model with a double-folding potential. The set of optical parameters selected for the system 9,11 Li (13 AMeV) + Si is given. The presence of neutron halo of 11 Li nucleus was taken into account by using adjusted values for the parameters r R and a R . The 28 Si nucleus is considered a rigid rotor, including the couplings involving the ground state and a first to excited states. The quadrupole deformation parameter was β 2 = - 0.24. The results for the scattering of 11 Li projectile on Si target at 13 AMeV energy are given with the parameters R match , I and J max taken from the Monte Carlo simulations with PACE code. We found that the contribution of elastic and inelastic scattering for background angles, between 80 angle - 180 angle is under 2%. The contribution of a inelastic scattering taken

  14. Effect of chevron nozzle penetration on aero-acoustic characteristics of jet at M = 0.8

    Science.gov (United States)

    Nikam, S. R.; Sharma, S. D.

    2017-12-01

    Aero-acoustic characteristics of a high-speed jet with chevron nozzles are experimentally investigated at a Mach number of 0.8. The main focus is to examine the effects of the extent of chevron penetration and its position in the mixing layer. Chevron nozzles with three different levels of penetration employed at three different longitudinal locations from the nozzle lip are tested, and the results are compared with those of a plain baseline nozzle. The chevrons are found to produce a lobed shear layer through the notched region, thereby increasing the surface area of the jet, particularly in the close vicinity of the nozzle, which increases the mixing and reduces the potential core length. This effect becomes more prominent with increasing penetration closer to the nozzle lip in the thinner mixing layer. Near field and far field noise measurements show distinctly different acoustic features due to chevrons. The chevrons are found to effectively shift the dominant noise source upstream closer to the nozzle. Present investigation proposes a simpler method for locating the dominant noise source from the peak of the centerline velocity decay rate. The overall noise levels registered along the jet edge immediately downstream of the chevrons are higher, but further downstream they are reduced in comparison with the plain baseline nozzle. Also, the chevrons beam the noise towards higher polar angles at higher frequencies. At shallow polar angles with respect to the jet axis in the far field, chevrons suppress the noise at low frequencies with increasing penetration, but for higher polar angles, while they continue to suppress the low frequency noise, at higher frequencies the trend is found to reverse. The noise measured in the near field close to the jet edge is composed of two components: acoustic and hydrodynamic. Of these two components, the chevrons are found to reduce the hydrodynamic component in comparison with the acoustic one.

  15. Effect of chevron nozzle penetration on aero-acoustic characteristics of jet at M = 0.8

    Energy Technology Data Exchange (ETDEWEB)

    Nikam, S R [K. J. Somaiya college of Engineering, Mumbai (India); Sharma, S D, E-mail: srnikam12@gmail.com [I.I.T. Bombay, Mumbai (India)

    2017-12-15

    Aero-acoustic characteristics of a high-speed jet with chevron nozzles are experimentally investigated at a Mach number of 0.8. The main focus is to examine the effects of the extent of chevron penetration and its position in the mixing layer. Chevron nozzles with three different levels of penetration employed at three different longitudinal locations from the nozzle lip are tested, and the results are compared with those of a plain baseline nozzle. The chevrons are found to produce a lobed shear layer through the notched region, thereby increasing the surface area of the jet, particularly in the close vicinity of the nozzle, which increases the mixing and reduces the potential core length. This effect becomes more prominent with increasing penetration closer to the nozzle lip in the thinner mixing layer. Near field and far field noise measurements show distinctly different acoustic features due to chevrons. The chevrons are found to effectively shift the dominant noise source upstream closer to the nozzle. Present investigation proposes a simpler method for locating the dominant noise source from the peak of the centerline velocity decay rate. The overall noise levels registered along the jet edge immediately downstream of the chevrons are higher, but further downstream they are reduced in comparison with the plain baseline nozzle. Also, the chevrons beam the noise towards higher polar angles at higher frequencies. At shallow polar angles with respect to the jet axis in the far field, chevrons suppress the noise at low frequencies with increasing penetration, but for higher polar angles, while they continue to suppress the low frequency noise, at higher frequencies the trend is found to reverse. The noise measured in the near field close to the jet edge is composed of two components: acoustic and hydrodynamic. Of these two components, the chevrons are found to reduce the hydrodynamic component in comparison with the acoustic one. (paper)

  16. Using Satellite Observations to Evaluate the AeroCOM Volcanic Emissions Inventory and the Dispersal of Volcanic SO2 Clouds in MERRA

    Science.gov (United States)

    Hughes, Eric J.; Krotkov, Nickolay; da Silva, Arlindo; Colarco, Peter

    2015-01-01

    Simulation of volcanic emissions in climate models requires information that describes the eruption of the emissions into the atmosphere. While the total amount of gases and aerosols released from a volcanic eruption can be readily estimated from satellite observations, information about the source parameters, like injection altitude, eruption time and duration, is often not directly known. The AeroCOM volcanic emissions inventory provides estimates of eruption source parameters and has been used to initialize volcanic emissions in reanalysis projects, like MERRA. The AeroCOM volcanic emission inventory provides an eruptions daily SO2 flux and plume top altitude, yet an eruption can be very short lived, lasting only a few hours, and emit clouds at multiple altitudes. Case studies comparing the satellite observed dispersal of volcanic SO2 clouds to simulations in MERRA have shown mixed results. Some cases show good agreement with observations Okmok (2008), while for other eruptions the observed initial SO2 mass is half of that in the simulations, Sierra Negra (2005). In other cases, the initial SO2 amount agrees with the observations but shows very different dispersal rates, Soufriere Hills (2006). In the aviation hazards community, deriving accurate source terms is crucial for monitoring and short-term forecasting (24-h) of volcanic clouds. Back trajectory methods have been developed which use satellite observations and transport models to estimate the injection altitude, eruption time, and eruption duration of observed volcanic clouds. These methods can provide eruption timing estimates on a 2-hour temporal resolution and estimate the altitude and depth of a volcanic cloud. To better understand the differences between MERRA simulations and volcanic SO2 observations, back trajectory methods are used to estimate the source term parameters for a few volcanic eruptions and compared to their corresponding entry in the AeroCOM volcanic emission inventory. The nature of

  17. Retrospective study of the evolution of nutritional, inflammatory and bacteriological profiles of patients suffering from inoperable aero-digestive duct tumour during sequential or concomitant chemo-radiotherapy

    International Nuclear Information System (INIS)

    Martin, L.; Brocard, C.; Coudray, C.; Pavlovitch, J.M.

    2010-01-01

    The authors report a retrospective study which aimed at analysing a cohort of consecutive patients in terms of clinic and biological aspects reflecting their nutritional and inflammatory status as well as the status of their buccal bacterial flora during a sequential or concomitant chemo-radiotherapy. The objective was to detect a possible difference between these both therapeutic modalities, and a possible relationship with toxicity. Several data have been collected for patients suffering from inoperable aero-digestive tract tumour: weight, body mass index, prealbumin, albumin, orosomucoid, C-reactive protein, PINI index, and buccal bacterial flora. The evolution of these nutritional biological criteria appears to depend on the treatment modality. Short communication

  18. Stability of two-degrees-of-freedom aero-elastic models with frequency and time variable parametric self-induced forces

    Czech Academy of Sciences Publication Activity Database

    Náprstek, Jiří; Pospíšil, Stanislav; Yau, J. D.

    2015-01-01

    Roč. 57, August (2015), s. 91-107 ISSN 0889-9746 R&D Projects: GA MŠk(CZ) LO1219; GA ČR(CZ) GC13-34405J Institutional support: RVO:68378297 Keywords : aero-elastic system * self-excited vibration * dynamic stability * Routh–Hurwitz conditions * flutter derivatives * divergence Subject RIV: JM - Building Engineering Impact factor: 1.709, year: 2015 http://dx.doi.org/10.1016/j.jfluidstructs.2015.05.010

  19. Mineralogy and characterization of deposited particles of the aero sediments collected in the vicinity of power plants and the open pit coal mine: Kolubara (Serbia).

    Science.gov (United States)

    Cvetković, Željko; Logar, Mihovil; Rosić, Aleksandra

    2013-05-01

    In this paper, particular attention was paid to the presence of aerosol solid particles, which occurred mainly as a result of exploitation and coal combustion in the thermal power plants of the Kolubara basin. Not all of the particles created by this type of anthropogenic pollution have an equal impact on human health, but it largely depends on their size and shape. The mineralogical composition and particle size distribution in the samples of aero sediments were defined. The samples were collected close to the power plant and open pit coal mine, in the winter and summer period during the year 2007. The sampling was performed by using precipitators placed in eight locations within the territory of the Lazarevac municipality. In order to characterize the sedimentary particles, several methods were applied: microscopy, SEM-EDX and X-ray powder diffraction. The concentration of aero sediments was also determined during the test period. Variety in the mineralogical composition and particle size depends on the position of the measuring sites, geology of the locations, the annual period of collecting as well as possible interactions. By applying the mentioned methods, the presence of inhalational and respiratory particles variously distributed in the winter and in the summer period was established. The most common minerals are quartz and feldspar. The presence of gypsum, clay minerals, calcite and dolomite as secondary minerals was determined, as well as the participation of organic and inorganic amorphic matter. The presence of quartz as a toxic mineral has a particular impact on human health.

  20. Neuronal protein gene product 9.5 (IEF SSP 6104) is expressed in cultured human MRC-5 fibroblasts of normal origin and is strongly down-regulated in their SV40 transformed counterparts

    DEFF Research Database (Denmark)

    Honoré, B; Rasmussen, H H; Vandekerckhove, J

    1991-01-01

    of proteins recovered from 2D gels we have identified PGP 9.5 UCH-L1 as polypeptide IEF SSP 6104 (Mr = 27,000, pI = 5.49) in the comprehensive 2D gel cellular protein database of human embryonal lung MRC-5 fibroblasts [(1989) Electrophoresis 10, 76 115; (1990) Electrophoresis 11, 1072 1113]. This protein...

  1. Long non-coding RNA TUG1 contributes to tumorigenesis of human osteosarcoma by sponging miR-9-5p and regulating POU2F1 expression.

    Science.gov (United States)

    Xie, Chu-Hai; Cao, Yan-Ming; Huang, Yan; Shi, Qun-Wei; Guo, Jian-Hong; Fan, Zi-Wen; Li, Ju-Gen; Chen, Bin-Wei; Wu, Bo-Yi

    2016-11-01

    Recent studies have shown that long non-coding RNAs (lncRNAs) have critical roles in tumorigenesis, including osteosarcoma. The lncRNA taurine-upregulated gene 1 (TUG1) was reported to be involved in the progression of osteosarcoma. Here, we investigated the role of TUG1 in osteosarcoma cells and the underlying mechanism. TUG1 expression was measured in osteosarcoma cell lines and human normal osteoblast cells by quantitative real-time PCR (qRT-PCR). The effects of TUG1 on osteosarcoma cells were studied by RNA interference in vitro and in vivo. The mechanism of competing endogenous RNA (ceRNA) was determined using bioinformatic analysis and luciferase assays. Our data showed that TUG1 knockdown inhibited cell proliferation and colony formation, and induced G0/G1 cell cycle arrest and apoptosis in vitro, and suppressed tumor growth in vivo. Besides, we found that TUG1 acted as an endogenous sponge to directly bind to miR-9-5p and downregulated miR-9-5p expression. Moreover, TUG1 overturned the effect of miR-9-5p on the proliferation, colony formation, cell cycle arrest, and apoptosis in osteosarcoma cells, which involved the derepression of POU class 2 homeobox 1 (POU2F1) expression. In conclusion, our study elucidated a novel TUG1/miR-9-5p/POU2F1 pathway, in which TUG1 acted as a ceRNA by sponging miR-9-5p, leading to downregulation of POU2F1 and facilitating the tumorigenesis of osteosarcoma. These findings may contribute to the lncRNA-targeted therapy for human osteosarcoma.

  2. Ablation in teeth with the free-electron laser around the absorption peak of hydroxyapatite (9.5 μm) and between 6.0 and 7.5 μm

    Science.gov (United States)

    Ostertag, Manfred; Walker, Rudolf; Weber, Heiner; van der Meer, Lex; McKinley, Jim T.; Tolk, Norman H.; Jean, Benedikt J.

    1996-04-01

    Pulsed IR laser ablation on dental hard substances was studied in the wavelength range between 9.5 and 11.5 micrometers with the Free-Electron Laser (FEL) in Nieuwegein/NL and between 6.0 and 7.5 micrometers with the FEL at Vanderbilt University in Nashville/TN. Depth, diameter and volume of the ablation crater were determined with a special silicon replica method and subsequent confocal laser topometry. The irradiated surfaces and the ejected debris were examined with an SEM 9.5 - 11.5 micrometers : depth, diameter and volume of the ablation crater are greater and the ablation threshold is lower for ablation with a wavelength corresponding to the absorption max. of hydroxyapatite (9.5 micrometers ), compared to ablation at wavelengths with lower absorption (10.5 - 11.5 micrometers ). For all wavelengths, no thermal cracking can be observed after ablation in dentine, however a small amount of thermal cracking can be observed after ablation in enamel. After ablation at 9.5 micrometers , a few droplets of solidified melt were seen on the irradiated areas, whereas the debris consisted only of solidified melt. In contrast, the surface and the debris obtained from ablation using the other wavelengths showed the natural structure of dentine 6.0 - 7.5 micrometers : the depth of the ablation crater increases and the ablation threshold decreases for an increasing absorption coefficient of the target material. Different tissue components absorbed the laser radiation of different wavelengths (around 6.0 micrometers water and collagen, 6.5 micrometers collagen and water, 7.0 micrometers carbonated hydroxyapatite). Nevertheless the results have shown no major influence on the primary tissue absorber.

  3. An Intron 9 CYP19 Gene Variant (IVS9+5G>A), Present in an Aromatase-Deficient Girl, Affects Normal Splicing and Is Also Present in Normal Human Steroidogenic Tissues.

    Science.gov (United States)

    Saraco, Nora; Nesi-Franca, Suzana; Sainz, Romina; Marino, Roxana; Marques-Pereira, Rosana; La Pastina, Julia; Perez Garrido, Natalia; Sandrini, Romolo; Rivarola, Marco Aurelio; de Lacerda, Luiz; Belgorosky, Alicia

    2015-01-01

    Splicing CYP19 gene variants causing aromatase deficiency in 46,XX disorder of sexual development (DSD) patients have been reported in a few cases. A misbalance between normal and aberrant splicing variants was proposed to explain spontaneous pubertal breast development but an incomplete sex maturation progress. The aim of this study was to functionally characterize a novel CYP19A1 intronic homozygote mutation (IVS9+5G>A) in a 46,XX DSD girl presenting spontaneous breast development and primary amenorrhea, and to evaluate similar splicing variant expression in normal steroidogenic tissues. Genomic DNA analysis, splicing prediction programs, splicing assays, and in vitro protein expression and enzyme activity analyses were carried out. CYP19A1 mRNA expression in human steroidogenic tissues was also studied. A novel IVS9+5G>A homozygote mutation was found. In silico analysis predicts the disappearance of the splicing donor site in intron 9, confirmed by patient peripheral leukocyte cP450arom and in vitro studies. Protein analysis showed a shorter and inactive protein. The intron 9 transcript variant was also found in human steroidogenic tissues. The mutation IVS9+5G>A generates a splicing variant that includes intron 9 which is also present in normal human steroidogenic tissues, suggesting that a misbalance between normal and aberrant splicing variants might occur in target tissues, explaining the clinical phenotype in the affected patient. © 2015 S. Karger AG, Basel.

  4. Real-time analysis of ambient organic aerosols using aerosol flowing atmospheric-pressure afterglow mass spectrometry (AeroFAPA-MS)

    Science.gov (United States)

    Brüggemann, Martin; Karu, Einar; Stelzer, Torsten; Hoffmann, Thorsten

    2015-04-01

    Organic aerosol accounts for a major fraction of atmospheric aerosols and has implications on the earth's climate and human health. However, due to the chemical complexity its measurement remains a major challenge for analytical instrumentation.1 Here, we present the development, characterization and application of a new soft ionization technique that allows mass spectrometric real-time detection of organic compounds in ambient aerosols. The aerosol flowing atmospheric-pressure afterglow (AeroFAPA) ion source utilizes a helium glow discharge plasma to produce excited helium species and primary reagent ions. Ionization of the analytes occurs in the afterglow region after thermal desorption and results mainly in intact molecular ions, facilitating the interpretation of the acquired mass spectra. In the past, similar approaches were used to detect pesticides, explosives or illicit drugs on a variety of surfaces.2,3 In contrast, the AeroFAPA source operates 'online' and allows the detection of organic compounds in aerosols without a prior precipitation or sampling step. To our knowledge, this is the first application of an atmospheric-pressure glow discharge ionization technique to ambient aerosol samples. We illustrate that changes in aerosol composition and concentration are detected on the time scale of seconds and in the ng-m-3 range. Additionally, the successful application of AeroFAPA-MS during a field study in a mixed forest region in Central Europe is presented. Several oxidation products of monoterpenes were clearly identified using the possibility to perform tandem MS experiments. The acquired data are in agreement with previous studies and demonstrate that AeroFAPA-MS is a suitable tool for organic aerosol analysis. Furthermore, these results reveal the potential of this technique to enable new insights into aerosol formation, growth and transformation in the atmosphere. References: 1) IPCC, 2013: Summary for Policymakers. In: Climate Change 2013: The

  5. Parallelization of the unstructured Navier-stoke solver LILAC for the aero-thermal analysis of a gas-cooled reactor

    International Nuclear Information System (INIS)

    Kim, J. T.; Kim, S. B.; Lee, W. J.

    2004-01-01

    Currently lilac code is under development to analyse thermo-hydraulics of the gas-cooled reactor(GCR) especially high-temperature GCR which is one of the gen IV nuclear reactors. The lilac code was originally developed for the analysis of thermo-hydraulics in a molten pool. And now it is modified to resolve the compressible gas flows in the GCR. The more complexities in the internal flow geometries of the GCR reactor and aero-thermal flows, the number of computational cells are increased and finally exceeds the current computing powers of the desktop computers. To overcome the problem and well resolve the interesting physics in the GCR it is conducted to parallels the lilac code by the decomposition of a computational domain or grid. Some benchmark problems are solved with the parallelized lilac code and its speed-up characteristics by the parallel computation is evaluated and described in the article

  6. Futurepath: The Story of Research and Technology at NASA Lewis Research Center. Structures for Flight Propulsion, ARC Sprayed Monotape, National Aero-Space Plane

    Science.gov (United States)

    1989-01-01

    The story of research and technology at NASA Lewis Research Center's Structures Division is presented. The job and designs of the Structures Division needed for flight propulsion is described including structural mechanics, structural dynamics, fatigue, and fracture. The video briefly explains why properties of metals used in structural mechanics need to be tested. Examples of tests and simulations used in structural dynamics (bodies in motion) are briefly described. Destructive and non-destructive fatigue/fracture analysis is also described. The arc sprayed monotape (a composite material) is explained, as are the programs in which monotape plays a roll. Finally, the National Aero-Space Plane (NASP or x-30) is introduced, including the material development and metal matrix as well as how NASP will reduce costs for NASA.

  7. Results from the ASPIRE study for breast reconstruction utilizing the AeroForm™ patient controlled carbon dioxide-inflated tissue expanders.

    Science.gov (United States)

    Connell, Tony F

    2015-09-01

    Therapeutic or prophylactic mastectomy is often indicated for women with breast cancer, or for those at a high risk of developing cancer due to familial history or genetic mutations. Favorable aesthetic and psychological results make prosthetic reconstruction of the breast with placement of tissue expanders followed by permanent implant a popular choice for women diagnosed with breast cancer. This study describes the results of the ASPIRE trial, the objective of which was to provide supportive data to demonstrate the performance and safety of the AeroForm™ System in a population with broader selection criteria than previous studies. Results of the earlier PACE clinical studies (PACE 1 and 2) demonstrated that the AeroForm™ System could be used safely and effectively to achieve the desired expansion necessary for successful breast reconstruction. In the current ASPIRE trial described in the paper, performance of the device was evaluated by successful tissue expansion and exchange to breast implant(s) unless precluded by a non-device related event. Safety data was evaluated based on reported adverse events. A prospective, single center, open-label study in which subjects who met the inclusion criteria and agreed to participate were enrolled and implanted with the AeroForm expander either at the time of mastectomy (immediate) or sometime after mastectomy (delayed). In the event of a bilateral procedure, the expander was implanted in each side. Subjects were followed until the explant of the tissue expander(s) and exchange for silicone or saline breast implant(s). Thirty-four expanders were placed in 21 subjects in the clinical trial; the average age of subjects was 49.7 ± 8.6 years with average BMI of 26.1 ± 4.7. Bilateral procedures accounted for 62% of the total and 88% of the reconstructions were completed with a latissimus dorsi flap (anterior approach) per the investigators standard procedure. Four (12%) of the cases (12%) were completed in two subjects

  8. New aero-gravity results from the Arctic: Linking the latest Cretaceous-early Cenozoic plate kinematics of the North Atlantic and Arctic Ocean

    DEFF Research Database (Denmark)

    Døssing, Arne; Hopper, J.R.; Olesen, Arne Vestergaard

    2013-01-01

    The tectonic history of the Arctic Ocean remains poorly resolved and highly controversial. Details regarding break up of the Lomonosov Ridge from the Barents-Kara shelf margins and the establishment of seafloor spreading in the Cenozoic Eurasia Basin are unresolved. Significantly, the plate...... tectonic evolution of the Mesozoic Amerasia Basin is essentially unknown. The Arctic Ocean north of Greenland is at a critical juncture that formed at the locus of a Mesozoic three-plate setting between the Lomonosov Ridge, Greenland, and North America. In addition, the area is close to the European plate...... plateau against an important fault zone north of Greenland. Our results provide new constraints for Cretaceous-Cenozoic plate reconstructions of the Arctic. Key Points Presentation of the largest aero-gravity survey acquired over the Arctic Ocean Plate tectonic link between Atlantic and Arctic spreading...

  9. AeroADL: applying the integration of the Suomi-NPP science algorithms with the Algorithm Development Library to the calibration and validation task

    Science.gov (United States)

    Houchin, J. S.

    2014-09-01

    A common problem for the off-line validation of the calibration algorithms and algorithm coefficients is being able to run science data through the exact same software used for on-line calibration of that data. The Joint Polar Satellite System (JPSS) program solved part of this problem by making the Algorithm Development Library (ADL) available, which allows the operational algorithm code to be compiled and run on a desktop Linux workstation using flat file input and output. However, this solved only part of the problem, as the toolkit and methods to initiate the processing of data through the algorithms were geared specifically toward the algorithm developer, not the calibration analyst. In algorithm development mode, a limited number of sets of test data are staged for the algorithm once, and then run through the algorithm over and over as the software is developed and debugged. In calibration analyst mode, we are continually running new data sets through the algorithm, which requires significant effort to stage each of those data sets for the algorithm without additional tools. AeroADL solves this second problem by providing a set of scripts that wrap the ADL tools, providing both efficient means to stage and process an input data set, to override static calibration coefficient look-up-tables (LUT) with experimental versions of those tables, and to manage a library containing multiple versions of each of the static LUT files in such a way that the correct set of LUTs required for each algorithm are automatically provided to the algorithm without analyst effort. Using AeroADL, The Aerospace Corporation's analyst team has demonstrated the ability to quickly and efficiently perform analysis tasks for both the VIIRS and OMPS sensors with minimal training on the software tools.

  10. Solar Tower Experiments for Radiometric Calibration and Validation of Infrared Imaging Assets and Analysis Tools for Entry Aero-Heating Measurements

    Science.gov (United States)

    Splinter, Scott C.; Daryabeigi, Kamran; Horvath, Thomas J.; Mercer, David C.; Ghanbari, Cheryl M.; Ross, Martin N.; Tietjen, Alan; Schwartz, Richard J.

    2008-01-01

    The NASA Engineering and Safety Center sponsored Hypersonic Thermodynamic Infrared Measurements assessment team has a task to perform radiometric calibration and validation of land-based and airborne infrared imaging assets and tools for remote thermographic imaging. The IR assets and tools will be used for thermographic imaging of the Space Shuttle Orbiter during entry aero-heating to provide flight boundary layer transition thermography data that could be utilized for calibration and validation of empirical and theoretical aero-heating tools. A series of tests at the Sandia National Laboratories National Solar Thermal Test Facility were designed for this task where reflected solar radiation from a field of heliostats was used to heat a 4 foot by 4 foot test panel consisting of LI 900 ceramic tiles located on top of the 200 foot tall Solar Tower. The test panel provided an Orbiter-like entry temperature for the purposes of radiometric calibration and validation. The Solar Tower provided an ideal test bed for this series of radiometric calibration and validation tests because it had the potential to rapidly heat the large test panel to spatially uniform and non-uniform elevated temperatures. Also, the unsheltered-open-air environment of the Solar Tower was conducive to obtaining unobstructed radiometric data by land-based and airborne IR imaging assets. Various thermocouples installed on the test panel and an infrared imager located in close proximity to the test panel were used to obtain surface temperature measurements for evaluation and calibration of the radiometric data from the infrared imaging assets. The overall test environment, test article, test approach, and typical test results are discussed.

  11. 44 CFR 9.5 - Scope.

    Science.gov (United States)

    2010-10-01

    ... with the spirit of the Order to the extent practicable. For any action which is excluded from the... what is done by FIA or the Mitigation Directorate, in administering the National Flood Insurance... with the spirit of the Orders to the extent practicable: (i) The issuance of individual flood insurance...

  12. Evidence for monoclinic distortion in the ground state phase of underdoped La_1_._9_5Sr_0_._0_5CuO_4: A single crystal neutron diffraction study

    International Nuclear Information System (INIS)

    Singh, Anar; Schefer, Jürg; Frontzek, Matthias; Sura, Ravi; Conder, Kazimierz; Sibille, Romain F.; Ceretti, Monica; Paulus, Werner

    2016-01-01

    The existing controversy about the symmetry of the crystal structure of the ground state of the critical doped La_1_._9_5Sr_0_._0_5CuO_4 has been resolved by analyzing the single crystal neutron diffraction data collected between 5 and 730 K. We observed small but significant intensities for “forbidden” reflections given by extinction rules of the orthorhombic Bmab space group at low temperatures. A careful investigation of neutron diffraction data reveals that the crystal structure of La_1_._9_5Sr_0_._0_5CuO_4 at 5 K is monoclinic with B2/m (2/m 1 1) space group. The monoclinic structure emerges from the orthorhombic structure in a continuous way; however, the structure is stable below ∼120 K which agrees with other observed phenomena. Our results on symmetry changes are crucial for the interpretation of physical properties also in other high temperature superconductors with similar structures.

  13. Ultrasound Backscatter Microscopy Image-Guided Intraventricular Gene Delivery at Murine Embryonic Age 9.5 and 10.5 Produces Distinct Transgene Expression Patterns at the Adult Stage

    Directory of Open Access Journals (Sweden)

    Jiwon Jang

    2013-11-01

    Full Text Available In utero injection of a retroviral vector into the embryonic telencephalon aided by ultrasound backscatter microscopy permits introduction of a gene of interest at an early stage of development. In this study, we compared the tissue distribution of gene expression in adult mice injected with retroviral vectors at different embryonic ages in utero. Following ultrasound image-guided gene delivery (UIGD into the embryonic telencephalon, adult mice were subjected to whole-body luciferase imaging and immunohistochemical analysis at 6 weeks and 1 year postinjection. Luciferase activity was observed in a wide range of tissues in animals injected at embryonic age 9.5 (E9.5, whereas animals injected at E10.5 showed brain-localized reporter gene expression. These results suggest that mouse embryonic brain creates a closed and impermeable structure around E10. Therefore, by injecting a transgene before or after E10, transgene expression can be manipulated to be local or systemic. Our results also provide information that widens the applicability of UIGD beyond neuroscience studies.

  14. Application of serum microRNA-9-5p, 21-5p, and 223-3p combined with tumor markers in the diagnosis of non-small-cell lung cancer in Yunnan in southwestern China.

    Science.gov (United States)

    Yang, Yanlong; Chen, Kai; Zhou, Yongchun; Hu, Zaoxiu; Chen, Shuai; Huang, Yunchao

    2018-01-01

    Xuanwei City is located in late Permian coal-accumulating areas of the northeastern region of Yunnan Province. In China, morbidity and mortality from lung cancer are highest in Yunnan. Identifying useful circulating markers suitable for the diagnosis of lung cancer in this region is quite meaningful. In this study, we evaluated diagnostic roles of serum miR-9-5p, 21-5p, 223-3p, 135b-5p, 339-5p, and 501-5p in patients with non-small-cell lung cancer (NSCLC) in Yunnan. Moreover, we evaluated the diagnostic performance of several tumor markers, including carcinoembryonic antigen (CEA), cytokeratin 19 fragment 21-1 (CYFRA21-1), and squamous cell carcinoma-related antigen (SCC). Quantitative real-time polymerase chain reaction detected six miRNAs in the serum of 104 NSCLC patients and 50 cancer-free controls. Other markers, including CEA, CYFRA21-1, and SCC, in serum were also measured. The diagnostic ability of miRNAs and tumor markers was evaluated by receiver operating characteristic (ROC) curve analysis. The diagnostic performance of these serum markers was also evaluated in Xuanwei and non-Xuanwei subjects, because the etiological and the epidemiological characteristics of lung cancer in Xuanwei were quite different from those in other regions. Serum miR-9-5p, miR-21-5p, miR-223-3p, CEA, CYFRA21-1, and SCC were upregulated in NSCLC patients, compared with cancer-free controls. No significant difference was found in miR-135b-5p, miR-339-5p, and miR-501-5p expression. The area under ROC curves (AUCs) of miR-9-5p, miR-21-5p, miR-223-3p, CEA, CYFRA21-1, and SCC were 0.706, 0.765, 0.744, 0.749, 0.735, and 0.616, respectively. When combined, miRNAs and tumor markers yielded the highest diagnostic power, with AUC of 0.886, sensitivity of 82.69%, and specificity of 88.00%. In Xuanwei subjects, miR-223-3p and CEA may be suitable biomarkers to distinguish NSCLC from cancer-free states with AUCs of 0.752 and 0.791, respectively. The diagnostic power of the combination of mi

  15. A-Train Aerosol Observations Preliminary Comparisons with AeroCom Models and Pathways to Observationally Based All-Sky Estimates

    Science.gov (United States)

    Redemann, J.; Livingston, J.; Shinozuka, Y.; Kacenelenbogen, M.; Russell, P.; LeBlanc, S.; Vaughan, M.; Ferrare, R.; Hostetler, C.; Rogers, R.; hide

    2014-01-01

    We have developed a technique for combining CALIOP aerosol backscatter, MODIS spectral AOD (aerosol optical depth), and OMI AAOD (absorption aerosol optical depth) retrievals for the purpose of estimating full spectral sets of aerosol radiative properties, and ultimately for calculating the 3-D distribution of direct aerosol radiative forcing. We present results using one year of data collected in 2007 and show comparisons of the aerosol radiative property estimates to collocated AERONET retrievals. Use of the recently released MODIS Collection 6 data for aerosol optical depths derived with the dark target and deep blue algorithms has extended the coverage of the multi-sensor estimates towards higher latitudes. We compare the spatio-temporal distribution of our multi-sensor aerosol retrievals and calculations of seasonal clear-sky aerosol radiative forcing based on the aerosol retrievals to values derived from four models that participated in the latest AeroCom model intercomparison initiative. We find significant inter-model differences, in particular for the aerosol single scattering albedo, which can be evaluated using the multi-sensor A-Train retrievals. We discuss the major challenges that exist in extending our clear-sky results to all-sky conditions. On the basis of comparisons to suborbital measurements, we present some of the limitations of the MODIS and CALIOP retrievals in the presence of adjacent or underlying clouds. Strategies for meeting these challenges are discussed.

  16. Forecasting olive crop yields based on long-term aero biological data series and bio climatic conditions for the southern Iberian Peninsula

    Energy Technology Data Exchange (ETDEWEB)

    Aguilera, F.; Ruiz-Valenzuela, L.

    2014-06-01

    In the present study, bio-meteorological models for predicting olive-crop production in the southern Iberian Peninsula were developed. These covered a 16-year period: 1994-2009. The forecasting models were constructed using the partial least-squares regression method, taking the annual olive yield as the dependent variable, and both aero biological and meteorological parameters as the independent variables. Two regression models were built for the prediction of crop production prior to the final harvest at two different times of the year: July and November. The percentage variance explained by the models was between 83% and 93%. Through these forecasting models, the main factors that influence olive-crop yield were identified. Pollen index and accumulated precipitation, especially as rain recorded during the pre-flowering months, were the most important parameters for providing an explanation of fluctuations in fruit production. The temperature recorded during the two months preceding budburst was another important variable, which showed positive effects on the final yield. The July model that provides accurate predictions of fruit production eight months prior to the final harvest is proposed as an optimal model to forecast fruit produced by olive trees in western Mediterranean areas. (Author)

  17. Direct Aerosol Radiative Forcing from Combined A-Train Observations - Preliminary Comparisons with AeroCom Models and Pathways to Observationally Based All-sky Estimates

    Science.gov (United States)

    Redemann, J.; Livingston, J. M.; Shinozuka, Y.; Kacenelenbogen, M. S.; Russell, P. B.; LeBlanc, S. E.; Vaughan, M.; Ferrare, R. A.; Hostetler, C. A.; Rogers, R. R.; Burton, S. P.; Torres, O.; Remer, L. A.; Stier, P.; Schutgens, N.

    2014-12-01

    We describe a technique for combining CALIOP aerosol backscatter, MODIS spectral AOD (aerosol optical depth), and OMI AAOD (absorption aerosol optical depth) retrievals for the purpose of estimating full spectral sets of aerosol radiative properties, and ultimately for calculating the 3-D distribution of direct aerosol radiative forcing. We present results using one year of data collected in 2007 and show comparisons of the aerosol radiative property estimates to collocated AERONET retrievals. Use of the recently released MODIS Collection 6 data for aerosol optical depths derived with the dark target and deep blue algorithms has extended the coverage of the multi-sensor estimates towards higher latitudes. Initial calculations of seasonal clear-sky aerosol radiative forcing based on our multi-sensor aerosol retrievals compare well with over-ocean and top of the atmosphere IPCC-2007 model-based results, and with more recent assessments in the "Climate Change Science Program Report: Atmospheric Aerosol Properties and Climate Impacts" (2009). For the first time, we present comparisons of our multi-sensor aerosol direct radiative forcing estimates to values derived from a subset of models that participated in the latest AeroCom initiative. We discuss the major challenges that exist in extending our clear-sky results to all-sky conditions. On the basis of comparisons to suborbital measurements, we present some of the limitations of the MODIS and CALIOP retrievals in the presence of adjacent or underlying clouds. Strategies for meeting these challenges are discussed.

  18. Modeling, Analysis, and Control of a Hypersonic Vehicle with Significant Aero-Thermo-Elastic-Propulsion Interactions: Elastic, Thermal and Mass Uncertainty

    Science.gov (United States)

    Khatri, Jaidev

    This thesis examines themodeling, analysis, and control system design issues for scramjet powered hypersonic vehicles. A nonlinear three degrees of freedom longitudinal model which includes aero-propulsion-elasticity effects was used for all analyses. This model is based upon classical compressible flow and Euler-Bernouli structural concepts. Higher fidelity computational fluid dynamics and finite element methods are needed for more precise intermediate and final evaluations. The methods presented within this thesis were shown to be useful for guiding initial control relevant design. The model was used to examine the vehicle's static and dynamic characteristics over the vehicle's trimmable region. The vehicle has significant longitudinal coupling between the fuel equivalency ratio (FER) and the flight path angle (FPA). For control system design, a two-input two-output plant (FER - elevator to speed-FPA) with 11 states (including 3 flexible modes) was used. Velocity, FPA, and pitch were assumed to be available for feedback. Aerodynamic heat modeling and design for the assumed TPS was incorporated to original Bolender's model to study the change in static and dynamic properties. De-centralized control stability, feasibility and limitations issues were dealt with the change in TPS elasticity, mass and physical dimension. The impact of elasticity due to TPS mass, TPS physical dimension as well as prolonged heating was also analyzed to understand performance limitations of de-centralized control designed for nominal model.

  19. AQUA-motion domain and metaphorization patterns in European Portuguese: AQUA-motion metaphor in AERO-motion and abstract domains

    Directory of Open Access Journals (Sweden)

    Hanna Jakubowicz Batoréo

    2016-03-01

    Full Text Available The AQUA-motion verbs – as studied by Majsak & Rahilina 2003 and 2007, Lander, Majsak & Rahilina [2005] 2008, 2012 and 2013, and Divjak & Lemmens 2007, and in European Portuguese (EP by Batoréo, 2007, 2008, 2009; Batoréo et al., 2007; Casadinho, 2007 – allow typically metaphorical uses, which we postulate can be organized in patterns. Our study shows that in European Portuguese there are two metaphorization patterns to be observed: (i AQUA-motion metaphor in AERO-motion domain and (ii AQUA-motion metaphor in abstract domain (e.g. abundance, arts, politics, etc.. In the first case, where the target domain of the metaphorization is the air, in EP we navigate through a crowd or we float in a waltz, whereas in the second, where it is abstract, we swim in money or in blood, and politicians navigate at sea or face floating currency in finances. In the present paper we survey the EP verbs of AQUA-motion metaphors in non-elicited data from electronically available language corpora (cf. Linguateca. In some cases comparisons are made with typologically diferent languages (as, e.g. Polish, cf. Prokofjeva’s 2007, Batoréo 2009.

  20. Les premières phases d'édification du stratovolcan du Cantal (Massif central, France) entre 9,5 et 8,0Ma : géologie et géochimie du secteur de l'ÉlancèzeFirst stage of the Cantal stratovolcano (Massif Central, France) construction between 9.5 and 8.0Ma: geology and geochemistry of the Élancèze area

    Science.gov (United States)

    Legendre, Christelle; Caroff, Martial; Leyrit, Hervé; Nehlig, Pierre; Thièblemont, Denis

    2001-05-01

    Recent cartography of the Élancèze area resulted in the identification of a residual ancient topographic relief comprised of basaltic and intermediate silica-saturated lavas partly covered by brecciated formations, emplaced during the first stage of edification of the Cantal stratovolcano (9.5-8.0 Ma). The ancient relief has been the subject of a specified petrological study. Although the corresponding mineralogical and geochemical data are rather consistent with the assumption of a differentiation mainly governed by fractional crystallization, the study of some incompatible trace element diagrams suggests that this process cannot have occurred in closed-system. A model of crustal assimilation coupled with fractional crystallization involving an amphibole-bearing cumulate is proposed.

  1. Jõulukuusest saab Stroomi rannas skulptuur / Malle Pajula

    Index Scriptorium Estoniae

    Pajula, Malle, 1971-

    2002-01-01

    Tuleskulptuuri seavad kokku rootsi kunstnikud Gunnar Carl Nilsson ja Ola Öhlin, kes Rootsis asutasid tuleskulptorite seltsi. Tuleskulptuure teevad ka eesti kunstnikud ja üliõpilased. Süüdatakse 14. jaanuaril

  2. Digitaalallkirja seadus saab sisu / Aare Reivart

    Index Scriptorium Estoniae

    Reivart, Aare, 1968-

    2000-01-01

    Sideoperaatorid ja pangad hakkavad välja töötama ühtset avalikku võtme infrastruktuuri (PKI), mis võimaldab telefoni ja interneti vahendusel kasutada mitmesuguseid teenuseid kiiresti ja turvaliselt

  3. Tutanhamon saab uue viimse puhkepaiga / Allan Espenberg

    Index Scriptorium Estoniae

    Espenberg, Allan

    2005-01-01

    Egiptuses hakatakse ehitama hiigelsuurt muuseumi, mis eksponaatide kõrval mahutaks ka kunstiteoste restaureerimise töökodasid ja Ramses II 12 m kõrguse kuju. Muuseum tuleks Giza püramiididest põhja poole. Projekti autor Iirimaa arhitektuuribüroo Heneghan Peng Architects

  4. Kust saab edaspidi elektrit? / Marko Pomerants

    Index Scriptorium Estoniae

    Pomerants, Marko, 1964-

    2008-01-01

    Ilmunud ka: Eesti Eest = Za Estoniju : Izdanije objedinenija "Sojuz Otetshestva i Res Publica" 20. nov. 2008, lk. 5. Millest toodetakse elektrit Eestis lähema 20 aasta jooksul. Riigikogu keskkonnakomisjoni esimees peab end Eesti oma tuumaelektrijaama küsimuses pessimistiks, vähemalt selle valmimises lähemal 12-15 aastal

  5. Kunstihoones saab vastutustundlikult vahetuskaupa teha / Andris Feldmanis

    Index Scriptorium Estoniae

    Feldmanis, Andris, 1982-

    2006-01-01

    Tutvustatakse Andrea Creutzi kunstiprojekti "Varjatud ressursivoog", mis on osa Tallinna Kunstihoones eksponeeritavast näitusest "Kapital (See veab meid alt)". Näitus tegeleb alternatiivsete majandusmudelitega

  6. Taimne linn - fantaasia saab tegelikkuseks / Kadri Kalle

    Index Scriptorium Estoniae

    Kalle, Kadri, 1984-

    2009-01-01

    Belgia arhitektist Luc Schuitenist ja tema töödest Brüsselis 2009. a. suvel eksponeeritud näitusel "Vegetal City". Arhitekt pakub loovaid lähenemisi sellele, kuidas linnad võiksid rohkem sarnaneda looduslike elupaikadega. Juba 1970. aastatel ehitas ta maja, mis kasutab päikese- ja tuuleenergiat, tema ideekavandite hulka kuuluvad ka üllatava disainiga keskkonnasõbralikud sõidukid

  7. Noore teadlase preemia saab Jaan Raik

    Index Scriptorium Estoniae

    2004-01-01

    Vabariigi presidendi kultuurirahastu nõukogu otsustas tänavuse noore teadlase preemia anda Tallinna Tehnikaülikooli vanemteadurile, tehnikateaduste doktor Jaan Raik'ile. Ilmunud ka Pärnu Postimees, 2004/Dec/1, lk. 6 ; Mente et Manu, 2004/Dec/15, lk. 1

  8. Kõik hea saab kord otsa / Krista Kumberg

    Index Scriptorium Estoniae

    Kumberg, Krista, 1959-

    2010-01-01

    Arvustus: Rowling, J. K. Bard Beedle’i lood / ruunikirjas algteosest tõlkinud Hermione Granger, inglise keelest tõlkinud Krista Kaer. Tallinn : Varrak, 2009 ; Benedictus, David. Tagasi Saja Aakri Metsa. Tallinn : Fookus Meedia, 2009

  9. Tantsud Tartus - vaatajast saab looja / Andres Keil

    Index Scriptorium Estoniae

    Keil, Andres, 1974-

    2007-01-01

    Festivalide Draama ja Eclectica tantsulavastustest : Krõõt Juuraku "Once Upon", Kaja Kannu, Martins Eiche ja Aigars Aipinsi "Vabadus/Briviba" ja Mairika Plakso ja Margus Toomla "The story of M & M Part II"

  10. Eesti saab oma veekeskused / Priit Vare

    Index Scriptorium Estoniae

    Vare, Priit, 1975-

    1999-01-01

    Aastaks 2001 kerkivad Tartusse ja Pärnusse Eesti esimesed veekeskused. Tartu vee- ja tervisekeskuse ehitamine on alanud. Projekteerija: AS Tari. Ehitaja: AS Ehitusfirma Rand & Tuulberg. Pärnusse tahab Kristine Center rajada kümblushotelli hoonesse, millest pidi saama uus mudaravila. Kommenteerivad Tartu abilinnapea H. Astok, Kristine Centeri investeeringute juhataja E. Parelo.

  11. Tallinn saab uue linnaskulptuuri / Tarmo Michelson

    Index Scriptorium Estoniae

    Michelson, Tarmo, 1975-

    1998-01-01

    Ideekavandite võistluse võitjad: 1. preemia Angela Orgusaare skulptuur "Urban Egg", 2. preemia Lembit Palmi skulptuur "399" ja 3. preemia Leida Ilo töö "Majakas". Skulptuur püstitatakse Hoiupanga lähedale.

  12. Maailma parimat Iiri kohvi saab Eestis

    Index Scriptorium Estoniae

    2007-01-01

    Baristade maailmameistrivõistlustel Belgias saavutas Eesti parim kohvikubaarmen Helger Aava kohvikust C'est La Vie parima alkoholi sisaldava kohvijoogi Coffee in Good Spirit valmistamise erivõistlustel esimese koha

  13. Helsingi saab eestlaste disainitud pingid / Raivo Murde

    Index Scriptorium Estoniae

    Murde, Raivo

    2010-01-01

    Eesti ettevõtte Frog Industrial Designi kaubamärgi Extery pingid "Klaar" võitsid Helsingi avaliku ruumi mööblikonkursi. Tooteseeria autoriteks on Martin Pärn, Edina Dufala-Pärn, Sven Sõrmus ja Pent Talvet disainibüroost Iseasi. Žürii valis Exteri toodangust välja ka teisi linnaruumis kasutatavaid elemente. Eestlaste disainitud linnamööbel on eksponeeritud Helsingi sisustusmessil Habitare

  14. Kas Iisrael saab oma tahtmise? / Toomas Alatalu

    Index Scriptorium Estoniae

    Alatalu, Toomas, 1942-

    2006-01-01

    Autori hinnangul on Lähis-Ida sündmused hakanud tormiliselt arenema, mille võtmesündmuseks on Palestiina peaministri ja Hamasi ühe liidri Ismail Haniyehi tagasipöördumine oma esimeselt välisreisilt Iraani, Pärsia lahe riikidesse ja Sudaani

  15. Maksureformist saab valitsuse kirstunael / Kai Kalamees

    Index Scriptorium Estoniae

    Kalamees, Kai

    2005-01-01

    2006. aasta eelarve kokkupanemine ja eelarvestrateegia kinnitamine aastateks 2006-2009 võib aprillis-mais koalitsioonipartnerid taas konfliktini viia, kuna kahe järgneva aasta vältel ei ole võimalik samaaegselt langetada tulumaksu 20 protsendini ja täita koalitsioonileppe lubadusi. Lisad: Reformi juhatuses sisepinged; Maksureform

  16. SAAB Tackling the Black, Brown Male Crisis

    Science.gov (United States)

    Pluviose, David

    2007-01-01

    Increasingly, dropping out of high school is a one-way ticket to prison for Black men. Recent research conducted by sociologists Becky Pettit and Bruce Western indicates that 3 percent of Whites and 20 percent of Blacks born between 1965 and 1969 had served time in prison by their early thirties. The crisis among Black and Hispanic men mobilized…

  17. Verest saab vein : [luuletused] / Mare Osi

    Index Scriptorium Estoniae

    Osi, Mare

    2003-01-01

    Sisu: "Must üü nigu kaaren ..." ; Metamorfoos ; Pettumus ; Skeptiline ; Talisman ; Unetet latsepõli ; Meie kaits ; Sannaõhtu ; "Külmä süä lüüdi lõhki ..." ; "Egäl kevädil ...". Eluloolisi andmeid autori kohta lk. 193

  18. Eesti seep saab hoo sisse / Maria Ulfsak

    Index Scriptorium Estoniae

    Ulfsak, Maria, 1981-

    2003-01-01

    Kanal 2s algab uus kodumaine komöödiasari "Õpetajate tuba", mille käsikiri on Peep Pedmansonilt, lavastus Ivo Eensalult, näitlejad on Ita Ever, Eino Baskin, Madis Milling, Henrik Normann, Maria Klenskaja, Margus Tabor jt., tootjafirmaks "Ruut"

  19. Filmikunst saab igamehe bisniseks / Priit Pullerits

    Index Scriptorium Estoniae

    Pullerits, Priit, 1965-

    2000-01-01

    Eesti Aasta Film '99 tiitli saanud 26-aastase Marko Raadi "Esteetilistel põhjustel" näitab suundumust, et väga väikeste rahadega võivad andekad inimesed teha häid filme, mis konkureerivad suure eelarvega linateostega

  20. Ekspressi tellija saab rikkaliku kogumiku Eesti muusikat

    Index Scriptorium Estoniae

    2008-01-01

    Viimasel kaheksal nädalal on ajalehemüügikohtades Eesti Ekspressi vahel olnud Eesti artistide singelplaadid: Tõnis Mägi ja Noorkuu, Jana Kask, Metsatöll, HU?, Ithaka-Maria, Rainer Jancise muusika filmist "Mina olin siin", Toe Tag, Birgit Õigemeel. Selgunud on Eesti Ekspressi tellijatele jaanuari alguses saadetava singlikogumiku lisaartistid: Vaiko Eplik, Pedigree, Traffic, Slide-Fifty ja Lenna Kuurmaa, Smilers, Leslie Da Bass ja Singer-Vinger

  1. Ostetud saab vaid parim / Silvia Viidik

    Index Scriptorium Estoniae

    Viidik, Silvia, 1972-

    2010-01-01

    Maailma kaks suuremat kiibitootjat - Advanced Micro Devices ja Intel - alandasid oma kvartaliprognoose. Autor analüüsib, mis sellel turul toimub, ning ütleb, et enne tulemuste hooaega võiks infotehnoloogiasektorist huvitatud investor kaaluda pigem ettevõtteid, kes toodavad ka väga valivale kliendile sobivaid tooteid

  2. Kortermajast saab kena kodu / Mirja Adler

    Index Scriptorium Estoniae

    Adler, Mirja

    2005-01-01

    KredExi eluasemevaldkonna juht soovitab kortermaja renoveerimiseks julgelt laenu võtta, kuna see on ehitushindade pideva tõusu tõttu laenuvõtjale lõppkokkuvõttes odavam kui iseseisvalt remondiraha koguda. Tabelid: Kogumise ja laenu hinnatõusu võrdlus; KredExi käenduse maksumus

  3. Kassinurme saab Kassirabaks / Riina Mägi

    Index Scriptorium Estoniae

    Mägi, Riina, 1957-

    2006-01-01

    30. juulil esietendub Jõgeva Linna Teatri vabaõhulavastus "Kassirabal", milles teevad kaasa ka professionaalsed näitlejad Ülle Lichtfeldt, Ines Aru ja Luule Komissarov ning Jõgeva, Põltsamaa, Tallinna, Mäetaguse ja teiste paikade harrastusnäitlejad

  4. Indiast saab maailma rahvarohkeim riik / Tõnu Prei

    Index Scriptorium Estoniae

    Prei, Tõnu, 1950-

    2005-01-01

    ÜRO rahvastikuraporti andmeil on maakera elanike arv 2050. a. 9,1 miljardit, kusjuures poole 2,6-miljardilisest juurdekasvust annavad vaid 9 riiki - India, Pakistan, Nigeeria, Kongo, Bangladesh, Uganda, USA, Etioopia ja Hiina

  5. Kõlakojas saab kuulata suvemuusikat / Eevi Laanemaa

    Index Scriptorium Estoniae

    Laanemaa, Eevi, 1962-

    2009-01-01

    13. hooaega alustavast kontserdisarjast "Kuressaare "Suvemuusika"" (projektijuht Katre Roolaht, kunstiline juht dirigent Matis Männa): Kuressaare Muusikakooli brassansambli ja Nõmme Muusikakooli brassansambli kontsert 7. juunil, Kuressaare Linnaorkester koos koos Maria Väliga 20. juunil, Big Band Tartu koos laulusolist Kreet Stubenderiga 27. juunil, tšellokvartett C-Jam 12. juulil ja Talsi Brassband Lätist 17. juulil

  6. Meningokoki vastu saab end vaktsineerida / Ada Maltseva

    Index Scriptorium Estoniae

    Maltseva, Ada, 1970-

    2008-01-01

    Vt. ka Linnaleht : Tallinn : na russkom jazõke, Linnaleht : Tartu 16. jaan., lk. 7. Tervisekaitseinspektsiooni avalike suhete juht Iiris Saluri räägib meningokokknakkusest ning selle vastu vaktsineerimisest

  7. Salaselts saab presidendi koha / koost. Virgo Kruve

    Index Scriptorium Estoniae

    2004-01-01

    Yale'i ülikooli salaseltsi "Skull and Bones" mõjust Ameerika poliitikale, presidentide George Bush seeniori ja George W. Bushi kuulumisest mainitud ühingusse. Telesaate "60 minutit" materjalide põhjal

  8. Kõrgkoolidesse saab astuda Internetis / Liivia Mahlapuu

    Index Scriptorium Estoniae

    Mahlapuu, Liivia

    2006-01-01

    Käesoleval aastal kasutavad veebipõhist infosüsteemi SAIS tudengite vastuvõtmisel Audentese Ülikool, EBS, Kaitseväe Ühendatud Õppeasutused, TLÜ, Eesti Infotehnoloogia Kolledž, TTÜ, EKA, Tartu Tervishoiu Kõrgkool, TÜ, EMÜ, Tallinna Tervishoiu Kõrgkool ja Eesti-Ameerika Äriakadeemia

  9. Kõrgkoolidesse saab astuda internetis / Tarmu Kurm

    Index Scriptorium Estoniae

    Kurm, Tarmu

    2006-01-01

    Sel aastal kasutavad ühist sisseastumise infosüsteemi SAIS Audentese Ülikool, EBS, Kaitseväe Ühendatud Õppeasutused, TLÜ, Eesti Infotehnoloogia Kolledž, TTÜ, EKA, Tartu Tervishoiu Kõrgkool, TÜ, EMÜ, Tallinna Tervishoiu Kõrgkool ja Eesti-Ameerika Äriakadeemia

  10. Mis saab raamatupoest edasi? / Silvia Viidik

    Index Scriptorium Estoniae

    Viidik, Silvia, 1972-

    2010-01-01

    USA suurim raamatupoeketi Barnes & Noble majandustulemused näitavad, et e-raamatute ja e-lugejate müügi kasv on mõjutanud ka ettevõtte edukust, sundides raamatupoeketti oma strateegilisi valikuid ümber hindama

  11. AERO2S - SUBSONIC AERODYNAMIC ANALYSIS OF WINGS WITH LEADING- AND TRAILING-EDGE FLAPS IN COMBINATION WITH CANARD OR HORIZONTAL TAIL SURFACES (IBM PC VERSION)

    Science.gov (United States)

    Carlson, H. W.

    1994-01-01

    necessary only to add an identification record and the namelist data that are to be changed from the previous run. This code was originally developed in 1989 in FORTRAN V on a CDC 6000 computer system, and was later ported to an MS-DOS environment. Both versions are available from COSMIC. There are only a few differences between the PC version (LAR-14458) and CDC version (LAR-14178) of AERO2S distributed by COSMIC. The CDC version has one main source code file while the PC version has two files which are easier to edit and compile on a PC. The PC version does not require a FORTRAN compiler which supports NAMELIST because a special INPUT subroutine has been added. The CDC version includes two MODIFY decks which can be used to improve the code and prevent the possibility of some infrequently occurring errors while PC-version users will have to make these code changes manually. The PC version includes an executable which was generated with the Ryan McFarland/FORTRAN compiler and requires 253K RAM and an 80x87 math co-processor. Using this executable, the sample case requires about four hours to execute on an 8MHz AT-class microcomputer with a co-processor. The source code conforms to the FORTRAN 77 standard except that it uses variables longer than six characters. With two minor modifications, the PC version should be portable to any computer with a FORTRAN compiler and sufficient memory. The CDC version of AERO2S is available in CDC NOS Internal format on a 9-track 1600 BPI magnetic tape. The PC version is available on a set of two 5.25 inch 360K MS-DOS format diskettes. IBM AT is a registered trademark of International Business Machines. MS-DOS is a registered trademark of Microsoft Corporation. CDC is a registered trademark of Control Data Corporation. NOS is a trademark of Control Data Corporation.

  12. AERO2S - SUBSONIC AERODYNAMIC ANALYSIS OF WINGS WITH LEADING- AND TRAILING-EDGE FLAPS IN COMBINATION WITH CANARD OR HORIZONTAL TAIL SURFACES (CDC VERSION)

    Science.gov (United States)

    Darden, C. M.

    1994-01-01

    necessary only to add an identification record and the namelist data that are to be changed from the previous run. This code was originally developed in 1989 in FORTRAN V on a CDC 6000 computer system, and was later ported to an MS-DOS environment. Both versions are available from COSMIC. There are only a few differences between the PC version (LAR-14458) and CDC version (LAR-14178) of AERO2S distributed by COSMIC. The CDC version has one main source code file while the PC version has two files which are easier to edit and compile on a PC. The PC version does not require a FORTRAN compiler which supports NAMELIST because a special INPUT subroutine has been added. The CDC version includes two MODIFY decks which can be used to improve the code and prevent the possibility of some infrequently occurring errors while PC-version users will have to make these code changes manually. The PC version includes an executable which was generated with the Ryan McFarland/FORTRAN compiler and requires 253K RAM and an 80x87 math co-processor. Using this executable, the sample case requires about four hours to execute on an 8MHz AT-class microcomputer with a co-processor. The source code conforms to the FORTRAN 77 standard except that it uses variables longer than six characters. With two minor modifications, the PC version should be portable to any computer with a FORTRAN compiler and sufficient memory. The CDC version of AERO2S is available in CDC NOS Internal format on a 9-track 1600 BPI magnetic tape. The PC version is available on a set of two 5.25 inch 360K MS-DOS format diskettes. IBM AT is a registered trademark of International Business Machines. MS-DOS is a registered trademark of Microsoft Corporation. CDC is a registered trademark of Control Data Corporation. NOS is a trademark of Control Data Corporation.

  13. Synthesis and Characterization of Yttria-Stabilized Zirconia Nanoparticles Doped with Ytterbium and Gadolinium: ZrO2 9.5Y2O3 5.6Yb2O3 5.2Gd2O3

    Science.gov (United States)

    Bahamirian, M.; Hadavi, S. M. M.; Rahimipour, M. R.; Farvizi, M.; Keyvani, A.

    2018-06-01

    Defect cluster thermal barrier coatings (TBCs) are attractive alternatives to Yttria-stabilized zirconia (YSZ) in advanced applications. In this study, YSZ nanoparticles doped with ytterbium and gadolinium (ZrO2 9.5Y2O3 5.6Yb2O3 5.2Gd2O3 (ZGYbY)) were synthesized through a chemical co-precipitation and calcination method, and characterized by in situ high-temperature X-ray diffraction analysis in the temperature range of 25 °C to 1000 °C (HTK-XRD), thermogravimetric analysis, differential thermal analysis, Fourier transform infrared spectroscopy, Raman spectroscopy, and field emission scanning electron microscopy (FE-SEM). Precise cell parameters of t-prime phase and the best zirconia phase for TBC applications were calculated by Cohen's and Rietveld refinement methods. Optimum crystallization temperature of the precursor powder was found to be 1000 °C. Furthermore, FE-SEM results for the calcined ZGYbY powders indicated orderly particles of uniform shape and size with a small tendency toward agglomeration. Average lattice thermal expansion coefficient in the temperature range of 25 °C to 1000 °C was determined to be 31.71 × 10-6 K-1.

  14. Synthesis and Characterization of Yttria-Stabilized Zirconia Nanoparticles Doped with Ytterbium and Gadolinium: ZrO2 9.5Y2O3 5.6Yb2O3 5.2Gd2O3

    Science.gov (United States)

    Bahamirian, M.; Hadavi, S. M. M.; Rahimipour, M. R.; Farvizi, M.; Keyvani, A.

    2018-03-01

    Defect cluster thermal barrier coatings (TBCs) are attractive alternatives to Yttria-stabilized zirconia (YSZ) in advanced applications. In this study, YSZ nanoparticles doped with ytterbium and gadolinium (ZrO2 9.5Y2O3 5.6Yb2O3 5.2Gd2O3 (ZGYbY)) were synthesized through a chemical co-precipitation and calcination method, and characterized by in situ high-temperature X-ray diffraction analysis in the temperature range of 25 °C to 1000 °C (HTK-XRD), thermogravimetric analysis, differential thermal analysis, Fourier transform infrared spectroscopy, Raman spectroscopy, and field emission scanning electron microscopy (FE-SEM). Precise cell parameters of t-prime phase and the best zirconia phase for TBC applications were calculated by Cohen's and Rietveld refinement methods. Optimum crystallization temperature of the precursor powder was found to be 1000 °C. Furthermore, FE-SEM results for the calcined ZGYbY powders indicated orderly particles of uniform shape and size with a small tendency toward agglomeration. Average lattice thermal expansion coefficient in the temperature range of 25 °C to 1000 °C was determined to be 31.71 × 10-6 K-1.

  15. Search for the standard model Higgs boson in the ZH→νν¯bb¯ channel in 9.5 fb−1 of pp¯ collisions at √(s)=1.96 TeV

    International Nuclear Information System (INIS)

    Abazov, V.M.; Abbott, B.; Acharya, B.S.; Adams, M.; Adams, T.; Alexeev, G.D.; Alkhazov, G.; Alton, A.; Alverson, G.; Askew, A.; Atkins, S.; Augsten, K.; Avila, C.; Badaud, F.; Bagby, L.; Baldin, B.; Bandurin, D.V.; Banerjee, S.; Barberis, E.; Baringer, P.

    2012-01-01

    We present a search for the standard model Higgs boson in 9.5 fb -1 of pp ¯ collisions at √(s)=1.96 TeV collected with the D0 detector at the Fermilab Tevatron Collider. The final state considered contains a pair of b jets and is characterized by an imbalance in transverse energy, as expected from pp ¯ →ZH→νν ¯ bb ¯ production. The search is also sensitive to the WH→ℓνbb ¯ channel when the charged lepton is not identified. The data are found to be in good agreement with the expected background. For a Higgs boson mass of 125 GeV, we set a limit at the 95% C.L. on the cross section σ(pp ¯ →[Z/W]H), assuming standard model branching fractions, that is a factor of 4.3 times larger than the theoretical standard model value, while the expected factor is 3.9. The search is also used to measure a combined WZ and ZZ production cross section that is a factor of 0.94±0.31(stat)±0.34(syst) times the standard model prediction of 4.4 pb, with an observed significance of 2.0 standard deviations.

  16. Late xerostomia after intensity-modulated conformational radiotherapy of upper aero-digestive tract cancers: study 2004-03 by the head and neck oncology and radiotherapy Group (Gortec)

    International Nuclear Information System (INIS)

    Toledano, I.; Lapeyre, M.; Graff, P.; Serre, C.; Bensadoun, R.J.; Bensadoun, R.J.; Ortholan, C.; Calais, G.; Alfonsi, M.; Giraud, P.; Racadot, S.

    2010-01-01

    The authors report a retrospective assessment of late xerostomia according to the RTOG (Radiation Therapy Oncology Group) classification of the European Organization for Research and Treatment of Cancer (EORTC) among patients treated by intensity-modulated conformational radiotherapy (IMRT) and suffering from upper aero-digestive tract carcinomas of different stages. Some of these patients have bee operated, and some have been treated by chemotherapy. It appears that the IMRT results in a reduction of late xerostomia, and even in an absence of salivary toxicity. Short communication

  17. Characterization of Ni{sub 5}3.5-Fe{sub 1}9.5-Ga{sub 2}7 Ni{sub 5}3.5 ferromagnetic shape memory alloy produced by powder metallurgy; Caracterizacion de la aleacion Ni{sub 5}3.5-Fe{sub 1}9.5-Ga{sub 2}7 con memoria de forma ferromagnetica producida por metalurgia de polvos

    Energy Technology Data Exchange (ETDEWEB)

    Olmos, L.; Alvarado-Hernandez, F.; Omar Jimenez, H.; Vergara-Hernandez, J.; Arroyo Albiter, M.; Ochoa-Gamboa, R. A.

    2015-07-01

    The main drawback of ferromagnetic shape memory alloys fabricated through casting methods are its brittleness. In order to overcome this disadvantage, powder metallurgy is an ideal technique for the consolidation of many engineering parts. This paper is focused on the study of the milling and sintering effects of metallic powders over the evolution of the crystalline phases responsibly for the shape memory effect of these materials. To achieve this objective, ferromagnetic shape memory alloy powders (Ni{sub 5}3.5-Fe{sub 1}9.5-Ga{sub 2}7) were prepared from a cast ingot by mechanical milling at two different times of 30 and 60 minutes. The evolution of the phases was investigated through high temperature X-ray diffraction (HTXRD), whereas sintering was analyzed with dilatometry tests. X-ray studies showed that four different phases can be present depending on the particle size and temperature at which the heat treatment was performed. Coarser powders showed a B2 structure along with a γ phase while the finer showed a L21 structure when treated below 1173 K. Furthermore, finer powders had a modulated M14 martensitic structure after sintering at temperatures above 1273 K. The sintering of powders was slow and a mass diffusion mechanism was not clearly observed. (Author)

  18. Increased Expression of Herpes Virus-Encoded hsv1-miR-H18 and hsv2-miR-H9-5p in Cancer-Containing Prostate Tissue Compared to That in Benign Prostate Hyperplasia Tissue

    Directory of Open Access Journals (Sweden)

    Seok Joong Yun

    2016-06-01

    Full Text Available Purpose: Previously, we reported the presence of virus-encoded microRNAs (miRNAs in the urine of prostate cancer (CaP patients. In this study, we investigated the expression of two herpes virus-encoded miRNAs in prostate tissue. Methods: A total of 175 tissue samples from noncancerous benign prostatic hyperplasia (BPH, 248 tissue samples from patients with CaP and BPH, and 50 samples from noncancerous surrounding tissues from these same patients were analyzed for the expression of two herpes virus-encoded miRNAs by real-time polymerase chain reaction (PCR and immunocytochemistry using nanoparticles as molecular beacons. Results: Real-time reverse transcription-PCR results revealed significantly higher expression of hsv1-miR-H18 and hsv2-miRH9- 5p in surrounding noncancerous and CaP tissues than that in BPH tissue (each comparison, P<0.001. Of note, these miRNA were expressed equivalently in the CaP tissues and surrounding noncancerous tissues. Moreover, immunocytochemistry clearly demonstrated a significant enrichment of both hsv1-miR-H18 and hsv2-miR-H9 beacon-labeled cells in CaP and surrounding noncancerous tissue compared to that in BPH tissue (each comparison, P<0.05 for hsv1-miR-H18 and hsv2- miR-H9. Conclusions: These results suggest that increased expression of hsv1-miR-H18 and hsv2-miR-H95p might be associated with tumorigenesis in the prostate. Further studies will be required to elucidate the role of these miRNAs with respect to CaP and herpes viral infections.

  19. Towards the improvements of simulating the chemical and optical properties of Chinese aerosols using an online coupled model – CUACE/Aero

    Directory of Open Access Journals (Sweden)

    Chun-Hong Zhou

    2012-07-01

    Full Text Available CUACE/Aero, the China Meteorological Administration (CMA Unified Atmospheric Chemistry Environment for aerosols, is a comprehensive numerical aerosol module incorporating emissions, gaseous chemistry and size-segregated multi-component aerosol algorithm. On-line coupled into a meso-scale weather forecast model (MM5, its performance and improvements for aerosol chemical and optical simulations have been evaluated using the observations data of aerosols/gases from the intensive observations and from the CMA Atmosphere Watch network, plus aerosol optical depth (AOD data from CMA Aerosol Remote Sensing network (CARSNET and from Moderate Resolution Imaging Spectroradiometer (MODIS. Targeting Beijing and North China region from July 13 to 31, 2008, when a heavy hazy weather system occurred, the model captured the general variations of PM10 with most of the data within a factor of 2 from the observations and a combined correlation coefficient (r of 0.38 (significance level=0.05. The correlation coefficients are better at rural than at urban sites, and better at daytime than at nighttime. Chemically, the correlation coefficients between the daily-averaged modelled and observed concentrations range from 0.34 for black carbon (BC to 0.09 for nitrates with sulphate, ammonium and organic carbon (OC in between. Like the PM10, the values of chemical species are higher for the daytime than those for the nighttime. On average, the sulphate, ammonium, nitrate and OC are underestimated by about 60, 70, 96.0 and 10.8%, respectively. Black carbon is overestimated by about 120%. A new size distribution for the primary particle emissions was constructed for most of the anthropogenic aerosols such as BC, OC, sulphate, nitrate and ammonium from the observed size distribution of atmospheric aerosols in Beijing. This not only improves the correlation between the modelled and observed AOD, but also reduces the overestimation of AOD simulated by the original model size

  20. Adaptative control of aero-acoustic instabilities. Application to propulsion systems; Controle adaptatif des instabilites aeroacoustiques. Application aux systemes de propulsion

    Energy Technology Data Exchange (ETDEWEB)

    Mettenleiter, M.

    2000-02-15

    This work treats active adaptive control of aero-acoustic instabilities. In particular, we are interested in an application to solid propellant rockets. The study is part of the research program ASSM coordinated by CNES and ONERA and the aim is to increase the performance of the P230 segmented solid propellant boosters of the Ariane 5 rocket. The work has been carried out in collaboration with other partners of this program. The main objective of this study is the development of control algorithms, able to diminish low frequency instabilities encountered in propulsion systems. First, the instability phenomenon is analyzed in a simplified experimental setup and similarity is shown with instabilities observed in real propulsion systems. This study enables us to conceive adaptive control strategies, which have been tested on three different levels: - In a simplified dynamical simulation; - During an experimental study; - Using full numerical simulations. The three levels of application made it possible to study the behaviour of the different control strategies. We could show that the actuator signal modifies the behaviour of the system on the acoustic level. But as there is a strong interaction between the pressure fluctuations and the hydrodynamic behaviour, the flow structure is also modified by active control. This behaviour corresponds to the simplified model of the phenomenon, which has been used to define the control algorithms. The control action 'at the noise source' makes it possible to distinguish this kind of algorithms from schemes based on the anti-noise principle. After this first part, where we showed the feasibility of control, we particularly considered algorithms which can act in an unknown environment. The information about the system behaviour. which is necessary for convergence of the controller is now obtained in parallel during control. An identification off-line, used at the beginning of the research, is no longer necessary. Self

  1. What Controls the Vertical Distribution of Aerosol? Relationships Between Process Sensitivity in HadGEM3-UKCA and Inter-Model Variation from AeroCom Phase II

    Science.gov (United States)

    Kipling, Zak; Stier, Philip; Johnson, Colin E.; Mann, Graham W.; Bellouin, Nicolas; Bauer, Susanne E.; Bergman, Tommi; Chin, Mian; Diehl, Thomas; Ghan, Steven J.; hide

    2016-01-01

    The vertical profile of aerosol is important for its radiative effects, but weakly constrained by observations on the global scale, and highly variable among different models. To investigate the controlling factors in one particular model, we investigate the effects of individual processes in HadGEM3-UKCA and compare the resulting diversity of aerosol vertical profiles with the inter-model diversity from the AeroCom Phase II control experiment. In this way we show that (in this model at least) the vertical profile is controlled by a relatively small number of processes, although these vary among aerosol components and particle sizes. We also show that sufficiently coarse variations in these processes can produce a similar diversity to that among different models in terms of the global-mean profile and, to a lesser extent, the zonal-mean vertical position. However, there are features of certain models' profiles that cannot be reproduced, suggesting the influence of further structural differences between models. In HadGEM3-UKCA, convective transport is found to be very important in controlling the vertical profile of all aerosol components by mass. In-cloud scavenging is very important for all except mineral dust. Growth by condensation is important for sulfate and carbonaceous aerosol (along with aqueous oxidation for the former and ageing by soluble material for the latter). The vertical extent of biomass-burning emissions into the free troposphere is also important for the profile of carbonaceous aerosol. Boundary-layer mixing plays a dominant role for sea salt and mineral dust, which are emitted only from the surface. Dry deposition and below-cloud scavenging are important for the profile of mineral dust only. In this model, the microphysical processes of nucleation, condensation and coagulation dominate the vertical profile of the smallest particles by number (e.g. total CN >3 nm), while the profiles of larger particles (e.g. CN>100 nm) are controlled by the

  2. Formation of YxNd1-xBa2Cu3O7-δ (0≤x≤0.9) superconductors from an undercooled melt via aero-acoustic levitation

    International Nuclear Information System (INIS)

    Gustafson, D.E.; Hofmeister, W.H.; Bayuzick, R.J.; Nagashio, K.; Kuribayashi, K.

    2003-01-01

    This paper presents the results of rapid solidification experiments performed on the copper oxide superconductors Y x Nd 1-x Ba 2 Cu 3 O 7-δ (0≤x≤0.9). Spherical rare earth (RE) 123 specimens were levitated in O 2 using aero-acoustic levitation (AAL), melted with a laser, undercooled, and solidified. The peritectic transformation temperature for the reaction RE 2 BaCuO 5 +liquid→REBa 2 Cu 3 O 7-δ corresponding to the maximum recalescence temperature during solidification was determined. RE123 was formed directly from the melt for Y-Nd binary alloy compositions with Nd concentration greater than 20% (Y concentration less than 80%). A minimum in the peritectic transformation temperature for the Nd/Y123 system corresponding to a composition Y 0.3 Nd 0.7 123 was determined at 66 deg. C below the peritectic of pure Nd123

  3. Analysis of the role of the gene coding the Amyloid-Precursor Protein Binding Protein 1 (APP-BP1) in the radio-sensitivity of epidermoid carcinomas of the upper aero-digestive tract infected by the human papillomavirus

    International Nuclear Information System (INIS)

    Guihard, S.; Altmeyer, A.; Ramolu, L.; Macabre, C.; Abecassis, J.; Noel, G.; Jung, A.C.

    2010-01-01

    As the human papillomavirus (HPV) is at the origin of 25% of upper aero-digestive tract cancers, and as these tumours present an increased radio-sensitivity compared to other tumours, probably due to a greater transcriptional activity of p53, the authors report the study on the influence of a decrease of the expression of the APP-BP1 in these tumours which could favour a radio-induced apoptosis. By using a reverse transcriptase polymerase chain reaction (RT-PCR), they assessed the APP-BP1 expression levels as well as expression levels of transcriptions coding onco-proteins known to be over-expressed in HPV+ tumours. They compared the radio-sensitivities of HPV+ and HPV- cells, the first one appearing to be greater than the second one. Short communication

  4. Experimental and Numerical Investigation of the Outer Ring Cooling Concept in a Hybrid and in an All-Steel Ball Bearing Used in Aero-Engines by the Introduction of a Helical Duct

    Directory of Open Access Journals (Sweden)

    Michael Flouros

    2018-02-01

    Full Text Available Rolling element bearings for aero engine applications have to withstand very challenging operating conditions because of the high thermal impact due to elevated rotational speeds and loads. The high rate of heat generation in the bearing has to be sustained by the materials, and in the absence of lubrication these will fail within seconds. For this reason, aero engine bearings have to be lubricated and cooled by a continuous oil stream. When the oil has reached the outer ring it has already been heated up, thus its capability to remove extra heat from the outer ring is considerably reduced. Increasing the mass flow of oil to the bearing is not a solution since excess oil quantity would cause high parasitic losses (churning in the bearing chamber and also increase the demands in the oil system for oil storage, scavenging, cooling, hardware weight, etc. A method has been developed for actively cooling the outer ring of the bearing. The idea behind the outer ring cooling concept was adopted from fins that are used for cooling electronic devices. A spiral groove engraved in the outer ring material of the bearing would function as a fin body with oil instead of air as the cooling medium. The method was first evaluated in an all steel ball bearing and the results were a 50% reduction in the lubricating oil flow with an additional reduction in heat generation by more than 25%. It was then applied on a Hybrid ball bearing of the same size and the former results were reconfirmed. Hybrid bearings are a combination of steel made parts, like the outer ring, the inner ring, and the cage and of ceramic rolling elements. This paper describes the work done to-date as a follow up of the work described in, and demonstrates the potential of the outer ring cooling for a bearing. Friction loss coefficient, Nusselt number, and efficiency correlations have been developed on the basis of the test results and have been compared to correlations from other authors

  5. 32 CFR 9.5 - Procedures accorded the accused.

    Science.gov (United States)

    2010-07-01

    ... National Defense Department of Defense OFFICE OF THE SECRETARY OF DEFENSE MILITARY COMMISSIONS PROCEDURES FOR TRIALS BY MILITARY COMMISSIONS OF CERTAIN NON-UNITED STATES CITIZENS IN THE WAR AGAINST TERRORISM... defense, a copy of the charges in English and, if appropriate, in another language that the Accused...

  6. 38 CFR 9.5 - Payment of proceeds.

    Science.gov (United States)

    2010-07-01

    ..., discounted to the date of his or her death at the same rate used for inclusion of interest in the computation... remain unpaid will be discounted to the date of payment at the same rate used for inclusion of interest... is extended due to total disability converts the group insurance to an individual policy which is...

  7. 31 CFR 9.5 - Applications for investigation.

    Science.gov (United States)

    2010-07-01

    ..., both past and current. (c) Statistical material presented should be on a calendar-year basis for... domestic industry concerned with the article in question. (4) Pertinent statistics showing the quantities... competition created by imports of the article in question. (6) The effect, if any, of imports of the article...

  8. Formation of Y{sub x}Nd{sub 1-x}Ba{sub 2}Cu{sub 3}O{sub 7-{delta}} (0{<=}x{<=}0.9) superconductors from an undercooled melt via aero-acoustic levitation

    Energy Technology Data Exchange (ETDEWEB)

    Gustafson, D.E.; Hofmeister, W.H.; Bayuzick, R.J.; Nagashio, K.; Kuribayashi, K

    2003-01-20

    This paper presents the results of rapid solidification experiments performed on the copper oxide superconductors Y{sub x}Nd{sub 1-x}Ba{sub 2}Cu{sub 3}O{sub 7-{delta}} (0{<=}x{<=}0.9). Spherical rare earth (RE) 123 specimens were levitated in O{sub 2} using aero-acoustic levitation (AAL), melted with a laser, undercooled, and solidified. The peritectic transformation temperature for the reaction RE{sub 2}BaCuO{sub 5}+liquid{yields}REBa{sub 2}Cu{sub 3}O{sub 7-{delta}} corresponding to the maximum recalescence temperature during solidification was determined. RE123 was formed directly from the melt for Y-Nd binary alloy compositions with Nd concentration greater than 20% (Y concentration less than 80%). A minimum in the peritectic transformation temperature for the Nd/Y123 system corresponding to a composition Y{sub 0.3}Nd{sub 0.7}123 was determined at 66 deg. C below the peritectic of pure Nd123.

  9. SFRO booklets - The radiotherapy of cancers: of anal canal (Anus), brain, mediastinum, pancreas, lung, prostate, rectum, breast, upper aero-digestive tract (ENT cancers), cervix, endometrium (cervical cancers), and bladder for a better understanding of radiotherapy, sarcoma radiotherapy - To better understand your treatment

    International Nuclear Information System (INIS)

    Leroy, Thomas; Mornex, Francoise; Peiffert, Didier; Thariat, Juliette; Faivre, Jean-Christophe; Huguet, Florence; Vendrely, Veronique; Barillot, Isabelle; Janoray, Guillaume; Bibault, Jean-Emmanuel; Antoni, Delphine; Crehange, Gilles; Meillan, Nicolas; Pichon, Baptiste; Biau, Julian; Pointreau, Yoann; Mirabel, Xavier; Leysalle, Axel; Claren, Audrey; Cartier, Lysian; Chand, Mari-Eve; Jacob, Julian; Renard-Oldrini, Sophie; Le Pechoux, Cecile; Ducassou, Anne; Moureau-Zabotto, Laurence; Lagrange, Jean Leon; Molina, Sarah

    2016-07-01

    This document gathers several booklets which, for different types of cancers, propose information regarding the anatomy and location of the cancer, its diagnosis, possible treatments, secondary effects during treatment, some practical advices, issues related to the post-treatment period, associations and other resources which can be useful for patient information, and a glossary of the main terms used for this cancer and its treatment. Cancer types are anal canal (Anus), brain, mediastinum, pancreas, lung, prostate, rectum, breast, upper aero-digestive tract (ENT cancers), cervix, endometrium (cervical cancers), and bladder cancers

  10. Sinterability and conductivity of barium doped aluminium lanthanum oxyapatite La{sub 9.5}Ba{sub 0.5}Si{sub 5.5}Al{sub 0.5}O{sub 26.5} electrolyte of solid oxide fuel cells

    Energy Technology Data Exchange (ETDEWEB)

    Cao Xiaoguo [Faculty of Materials and Energy, Guangdong University of Technology, Guangzhou 510006, Guangdong (China); Jiang Sanping, E-mail: s.jiang@curtin.edu.au [Fuels and Energy Technology Institute and Department of Chemical Engineering, Curtin University, Perth, WA 6102 (Australia)

    2012-05-15

    Highlights: Black-Right-Pointing-Pointer Ba doping enhances the sintering and densification properties of aluminium lanthanum apatite. Black-Right-Pointing-Pointer Ba doping improves the oxide conductivity of aluminium lanthanum apatite. Black-Right-Pointing-Pointer The enhancement of Ba doping is mainly due to the significantly reduced grain boundary resistance of the aluminium lanthanum apatite. - Abstract: Apatite ceramics are interesting alternative solid oxide fuel cells (SOFCs) electrolytes because of their open structure for the transportation of oxide ions and their good chemical stability. This study reports the influence of barium doping on the microstructure, sinterability and oxide conductivity properties of the aluminium lanthanum oxyapatite La{sub 9.5}Ba{sub 0.5}Si{sub 5.5}Al{sub 0.5}O{sub 26.5}. SEM results show that lanthanum substitution with barium improves the sinterability of apatite ceramics. The barium doping also enhances the conductivity of the aluminium lanthanum silicates. The oxygen ion conductivity of La{sub 9.5}Ba{sub 0.5}Si{sub 5.5}Al{sub 0.5}O{sub 26.5} sintered at 1600 Degree-Sign C is 2.21 Multiplication-Sign 10{sup -2} S cm{sup -1} at 800 Degree-Sign C, higher than 9.81 Multiplication-Sign 10{sup -3} S cm{sup -1} of La{sub 10}Si{sub 5}AlO{sub 26.5} sample prepared under the same conditions. The results in the present study demonstrate that doping Ba on the La site for aluminium lanthanum oxyapatite reduces the sintering temperature and improves the ion conductivity. The enhancement of Ba dopant is mainly on the improvement of the densification and thus substantially reduced grain boundary resistance of aluminium lanthanum oxyapatite particularly at low temperatures.

  11. Ita Ever saab pojalt kingiks filmi / Ada Maltseva

    Index Scriptorium Estoniae

    Maltseva, Ada, 1970-

    2006-01-01

    Näitleja Ita Everi 75-ndaks sünnipäevaks jõuab ekraanile mängufilm "Vana daami visiit" : stsenaristid Roman Baskin, Ilmar Raag : režissöör Roman Baskin : MTÜ Kell Kümme koostöös ETV ja Exitfilmiga, Kultuurkapital. Filmi võtteplatsil toimunust

  12. Siseminister Pihl saab arvestada 300 lisamiljoniga / Tuuli Koch

    Index Scriptorium Estoniae

    Koch, Tuuli

    2008-01-01

    2009. aasta riigieelarve koostamisel tegi rahandusministeerium 3,5 miljardi krooni suuruse lisapakkumise, millest 300 miljonit peaks pehmendama siseministeeriumi koondamise ja kokkuhoiu stsenaariumi. Lisa: Must stsenaarium

  13. Saksa-Poola umbusk saab tuult tiibadesse / Jeroen Bult

    Index Scriptorium Estoniae

    Bult, Jeroen

    2005-01-01

    Uute valitsuste ametisseastumine Berliinis ja Poolas võib halvendada Saksa-Poola suhteid. Uut konservatiivset Poola valitsust iseloomustab euroskeptilisus ja Ameerika-meelsus, vähenenud on ka Saksamaa kantsleri Angela Merkeli kriitika Venemaa suhtes. Lisa: Pinged

  14. Internetireklaami odavast hinnast saab varsti ajalugu / Villu Zirnask

    Index Scriptorium Estoniae

    Zirnask, Villu, 1966-

    2006-01-01

    Delfi juhatuse esimehe Ville Jehe hinnangul toimub internetireklaami hinna tõus - umbes 20% aastas - vähemalt seni, kuni see on jõudnud telereklaami hinnaga lähedasele tasemele. Ühispanga turustusosakonna asedirektor Merike Kukk, online-reisibüroo bookinghouse.net turundusjuht Jane Ild interneti- ja telereklaami kasutamisest. Lisad. Diagrammid

  15. Eesti ja USA kaitsekoostöö saab uue aluspaberi

    Index Scriptorium Estoniae

    2017-01-01

    Valitsus kiitis eilsel istungil heaks Eesti ja Ameerika Ühendriikide valitsuse kaitsekoostöö kokkuleppe ning volitas kaitseminister Margus Tsahknat allkirjastama selle USA suursaadikuga Eestis. Leppe peab ratifitseerima ka riigikogu

  16. Lauri Liipa : alati saab paremini / Lauri Liipa ; interv. Jaana Pikalev

    Index Scriptorium Estoniae

    Liipa, Lauri, 1972-

    2007-01-01

    Ilmunud ka: Delovõje Vedomosti 12. dets. lk. 19. AS TNT Express Worldwide Eesti uus juht Lauri Liipa vastab küsimustele ettevõtte juhtimise ja ettevõtte rollist kiirkullerteenuste pakkumisel. Lisa: CV: Lauri Liipa

  17. Saaremaalt saab heinaseemet igale maitsele / Jana Rand ; kommenteerinud Hindrek Older

    Index Scriptorium Estoniae

    Rand, Jana, 1963-

    2016-01-01

    Saaremaal Laadjala külas tegutsev OÜ Saaremaa Seeme on Eesti suurim heinaseemne kasvataja, aga mitte erakordselt head looduslikud tingimused pole ettevõtte edu taganud, vaid aastakümnetega omandatud kogemused ja terve Sauna pere pühendunud töö. Vestlusest Arli Saunaga

  18. Riigilt saab toetust senisest rohkem inimesi / Heljo Pikhof

    Index Scriptorium Estoniae

    Pikhof, Heljo, 1958-

    2001-01-01

    Ilmunud ka: Meie Maa, 30. okt. 2001, lk. 2; Vooremaa, 30. okt. 2001, lk. 2; Koit, 30. okt. 2001, lk. 6; Lääne Elu, 30. okt. 2001, lk. 4. Vastuseks M. Treiali art.-le üle 80-aastastele pensionilisa maksmise kohta. Vanus ei ole objektiivne alus, et lisaraha maksta. Uuest toetuste süsteemist. Autor: Rahvaerakond Mõõdukad

  19. Eesti keele oskust saab ise mõõta

    Index Scriptorium Estoniae

    2009-01-01

    Eesti keele veebipõhistest testidest, mis lihtsustab nii kursuse- kui eksamivalikut. Keeleoskust testitakse viie Euroopa Liidus kasutatava keeletaseme ulatuses: tasemest A1 tasemeni C1. Veebikeskkond valmis integratsiooni sihtasutuse, riikliku eksami- ja kvalifikatsioonikeskuse, Juku Lab OÜ ning Tallinna Ülikooli koostöös

  20. Kuressaare linna uueks vapilaevaks saab miinijahtija Admiral Cowan / Raul Vinni

    Index Scriptorium Estoniae

    Vinni, Raul

    2008-01-01

    Eesti mereväe uusim alus, miinijahtija Admiral Cowan, hakkab Kuressaare sõpruslaevana kandma linna vappi. Juuresoleval fotol kuninganna Elizabeth II ja president Toomas Hendrik Ilves 20. oktoobril 2006 avamas Eesti uue miinijahtija Admiral Cowani vappi

  1. Saksamaa endine valitsusjuht saab gaasijuhtme eest pahandada / Kaivo Kopli

    Index Scriptorium Estoniae

    Kopli, Kaivo

    2005-01-01

    Saksamaa opositsioonipoliitikud ning välismaa meedia kritiseerivad Saksa endise kantsleri Gerhard Schröderi asumist Vene-Saksa gaasijuhet rajava firma etteotsa. Korruptsiooni jälgiva organisatsiooni Transparency International Saksamaa esindaja hinnang

  2. Pindalatoetusi saab tänavu taotleda maikuus / Heli Raamets

    Index Scriptorium Estoniae

    Raamets, Heli, 1975-

    2005-01-01

    Sama ka Vali Uudised 27. aprill 2005, lk. 7 ; Vooremaa : Palamuse Valla Teataja 30. aprill 2005, lk. 3 ; Vooremaa : Pala Teataja 3. mai 2005, lk. 2 artiklis pealkiri kujul: Pindalatoetuse taotlusi ootab PRIA mais ; Vooremaa : Jõgeva Valla Teataja 7. mai 2005, lk. 3 ; Vooremaa : Saare Valla Teataja 14. mai 2005, lk. 2 artiklis pealkiri kujul: PRIA ootab pindalatoetuse taotlusi

  3. Kui klassikaaslasest saab aastaks sinu boss / Sirje Pärismaa

    Index Scriptorium Estoniae

    Pärismaa, Sirje, 1958-

    2014-01-01

    Õpilasfirmade võistlusest. Tänavu võitis Tallinna Õismäe Vene Lütseumi õpilasfirma DK Koolitus, kes hakkas pakkuma algkoolilastele suhtlemisabi. 2. koht - Tallinna 21. Kooli võistkond EasyClip, 3. koht - Tallinna Reaalkooli võistkond Sants

  4. Eesti saab veel ühe monumendi / Eric A. Johnson

    Index Scriptorium Estoniae

    Johnson, Eric A.

    2008-01-01

    Eesti Vabadussõjas (1918-1920) osalesid peale soomlaste, rootslaste, taanlaste ja inglaste ka ameeriklased, kes olid enamuses Ameerika Punase Risti vabatahtlikud. Monument, mis plaanitakse valmis saada aasta lõpuks, hakkab seisma Tallinna kaitseväe kalmistul. Ilmunud ka: Linnaleht : na russkom jazõke, 23. mai 2008, lk 9 (V Estonii pojavitsja eshtshjo odin monument)

  5. Saabism and Saabists : An ethnographic analysis of Saab culture

    NARCIS (Netherlands)

    Maly, Ico

    Both Simmel and Goffman were deeply persuaded that the big things in society, in actual observable reality are made up of a dynamic and complex system of interlocking and interacting small things. In this paper, I wish to examine the online-offline communicative and semiotic practices of one such

  6. Parim, mida saab raha eest - hakka Staliniks / Jelena Skulskaja

    Index Scriptorium Estoniae

    Skulskaja, Jelena, 1950-

    2004-01-01

    Vene Kinematografistide Liidu esimehe valimistest. Vassili Aksjonovi romaani "Moskva saaga" ekraniseeringus Stalini rolli kinnitatud Moskva panga omaniku Vladimir Mironovi tööst rolliga. Venemaal on suurenenud huvi ajaloolise isiku, Grigori Rasputini vastu

  7. Kinnisvara pealt saab teenida seda ostmata / Romet Kreek

    Index Scriptorium Estoniae

    Kreek, Romet, 1972-

    2003-01-01

    Autor tutvustab võimalust investeerida kinnisvarasse läbi kinnisvara haldavate ettevõtete ehk REIT-ide, mille aktsiad on börsil kaubeldavad. Diagramm: REITide tootlus on ületanud aktsiaindeksite oma

  8. Ladina-Ameerika saab elektroonilise valuuta / Allan Espenberg

    Index Scriptorium Estoniae

    Espenberg, Allan

    2008-01-01

    Ladina-Ameerika riikide Venezuela, Kuuba, Boliivia, Hondurase, Nicaragua, Dominica ja Ecuadori ühendus ALBA on alustanud ettevalmistustega ühise virtuaalse valuuta, sucre, sisseseadmiseks ning ühtse majandus- ja rahandustsooni loomiseks

  9. ELi 52 miljardist saab lõviosa keskkond / Hindrek Riikoja

    Index Scriptorium Estoniae

    Riikoja, Hindrek

    2006-01-01

    Ilmunud ka: Postimees : na russkom jazõke 13. veebr. lk. 3. Euroopa Liidu struktuurifondidest Eestile aastateks 2007-2013 eraldatavast 52 miljardist kroonist läheb esialgse kava kohaselt 13,4 miljardit krooni keskkonnale, 11 miljardit haridusküsimuste lahendamiseks ning 11,8 miljardit ettevõtluse ja teaduse arendamiseks. Diagramm: Euroraha saajad

  10. Mis saab Eesti maaelust 2013. aastal? / Kalev Kotkas

    Index Scriptorium Estoniae

    Kotkas, Kalev, 1960-

    2007-01-01

    Ilmunud ka: Nädaline, 14. juuli 2007, lk. 5; Meie Maa, 13. juuli 2007, lk. 2; Järva Teataja, 17. juuli 2007, lk. 2; Valgamaalane, 17. juuli 2007, lk. 2; Hiiu Leht, 17. juuli 2007, lk. 2; Põhjarannik, 13. juuli 2007, lk. 3; Severnoje Poberezhje, 13. juuli 2007, lk. 3; Sõnumitooja, 18. juuli 2007, lk. 2; Pärnu Postimees, 19. juuli 2007, lk. 15; Lääne Elu, 19. juuli 2007, lk. 2; Võrumaa Teataja, 17. juuli 2007, lk. 2; Virumaa Teataja, 20. juuli 2007, lk. 11; Vooremaa, 19. juuli 2007, lk. 2; Sakala, 25. juuli 2007, lk. 2. Autor arutleb maaelu arengukava 2007-2013 meetmete võimaluse üle põllumajanduse konkurentsivõimet parandada ning hoiatab riigikontrolli maaelu käsitleva auditi ja selles prognoositavate majandusraskuste võimalike kaasmõjude eest noorte elukutsevalikule

  11. Tagasivõidetud Volta kvartalist saab autovaba keskkond / Urmas Oja

    Index Scriptorium Estoniae

    Oja, Urmas, 1981-2012

    2007-01-01

    Tallinna Volta kvartali arhitektuurikonkursist. I koht - soome arhitektuuribüroo AW2 Arkkitehdit. II koht - arhitektuuribüroo Kosmos. III koht - KOKO Arhitektid. Osalesid veel arhitektuuribüroo Muru & Pere ning arhitektuuribüroo Ehala & Irik. Žürii koosseis. Küsimustele vastab võidutöö autor Matti Anttila

  12. Venemaast saab pehme impeerium / Leonid Gozman ; interv. Vallo Toomet

    Index Scriptorium Estoniae

    Gozman, Leonid

    2003-01-01

    Venemaa Ühendatud Energiasüsteemide juhatuse liige Leonid Gozman vastab küsimustele, mis puudutavad riske äriajamisel Venemaaga, Eesti liitumist EL-iga, Kremli suhtumist Venemaa oligarhidesse, varanduslikku kihistumist, poliitilist arengut Venemaal

  13. Põltsamaa saab korraga kaheksa graniidist kuju / Risto Berendson

    Index Scriptorium Estoniae

    Berendson, Risto, 1975-

    2004-01-01

    Rahvusvahelise graniitskulptuuri festivali kahe kuu töö tulemusel kujuneb Põltsamaa Sõpruse park skulptuuripargiks. Tauno Kangro, Art Allmäe, Algirdas Kuzma temaatilistest skulptuuridest. Kohale tulemata jäänud skulptorite taiesed valmistas jooniste põhjal kohalik kiviraidur Madis Roio

  14. Vaid "rikas" tallinlane saab toitu valida / Vesta Reest

    Index Scriptorium Estoniae

    Reest, Vesta, 1971-

    1999-01-01

    Eestis toodetud kaupa ostavad Eesti keskmisest jõukamad Tallinna elanikud, mitte kõik eestlased. Ilmunud ka: Molodjozh Estonii, 3. juuli 1999, lk. 10; Den za Dnjom, 9. juuli 1999, lk. 14-15; Vesti : Nedelja Pljuss, 1. juuli 1999, lk. 11

  15. Polder saab Natura-alaks / Mati Määrits

    Index Scriptorium Estoniae

    Määrits, Mati, 1958-

    2003-01-01

    Brüsselis toimunud Elupaikade Komitee kokkusaamisel kiideti heaks 83 LIFE-Nature projekti taotlust. Eesti kaheksast projektist jäid sõelale Silma looduskaitseala ja Räpina poldri linnukaitseprojektid

  16. Raudteefirma omanik saab riigilt trahvinõude / Priit Rajalo

    Index Scriptorium Estoniae

    Rajalo, Priit, 1975-

    2005-01-01

    Eesti Raudtee omanikfirmat Baltic Rail Service (BRC) ähvardab 15 miljoni krooni suurune trahv, kuna valitsuse hinnangul on ettevõte investeerinud raudteeinfrastruktuuri vähem kui on ette nähtud erastamislepingus. Lisa: Investeeringud raudteesse

  17. Veemajandus saab jõudsalt areneda / Aare Lepaste

    Index Scriptorium Estoniae

    Lepaste, Aare, 1970-

    2004-01-01

    8. detsembril kirjutasid seitsme vee-ettevõtte esindajad, KIK-i juhataja ja keskkonnaminister alla Eesti suurimale keskkonnaprojektile. Projekti eesmärk on viia omavalitsuste veemajanduse infrastruktuur vastavusse EL-i direktiividega.

  18. Mis saab maaärist? / Ester Šank

    Index Scriptorium Estoniae

    Šank, Ester, 1956-

    2000-01-01

    Maaostu piirava seaduseelnõu Riigikogu menetlusest välja arvamist kommenteerib Vootele Hansen. Lisatud ka eelnõu autorite Jaanus Marrandi, Harri Õunapuu ja töörühma liikme Ain Kendra seisukohad

  19. Ravikindlustust saab igaüks / Merike Lees

    Index Scriptorium Estoniae

    Lees, Merike, 1976-

    2008-01-01

    Ilmunud ka: Delovõje Vedomosti 16. apr. lk. 14. Haigekassas on lihtne registreeruda suvalise firma töötajana ravikindlustatud isikuks. Vt. samas: Haiguslehtedega teenib tubli lisa; Vastutus langeb tööandjale; Ettekirjutusi vähe

  20. Pärnu saab esimese kõrghoone?

    Index Scriptorium Estoniae

    2006-01-01

    Pärnu kesklinna jõeäärse ala rahvusvahelise arhitektuurikonkursi võidutöö "Flood", mille autoriteks on itaalia arhitektid Francesco De Luca, Paolo Gori, Romolo Nati, Antonio Capasso ja Giuliana Mancinelli Bonafaccia. Ill.: 3 vaadet

  1. Liiklusõnnetusi saab vältida / Jarno Habicht

    Index Scriptorium Estoniae

    Habicht, Jarno, 1976-

    2004-01-01

    Liiklusõnnetuste vältimisest. Samas vastavad küsimusele jalgrattateede ja nende ohutuse kohta Prussakovi-nimelise rattaühingu liider Erko Valk, Tallinna abilinnapea Jüri Ratas ja Eesti Jalgratturite Liidu president Siim Kallas

  2. 2x väikesest saab suur / Varje Talivee

    Index Scriptorium Estoniae

    Talivee, Varje

    2011-01-01

    Sisearhitekt Aet Piel kujundas osavate kujundusvõtetega väikesest 43 m² kahetoalisest tüüpkorterist kaks ruumikalt mõjuvat tervikut, millest üks on elegantselt hall ning teine valge ja helge. Mõlemaid näidislahendusi esitleti sisustusmessil Interjöör 2011

  3. Püssi plaat saab 30aastaseks / Gerli Romanovitsh

    Index Scriptorium Estoniae

    Romanovitš, Gerli, 1977-

    2004-01-01

    Ilmunud ka: Severnoje Poberezhje, 22. dets. 2004, lk. 4. Aasta aega Šveitsi investeerimisfirmale Sorbes AG kuulunud Püssi Repo Vabrikud tähistab puitlaastvabrikute kombinaadi 30. sünnipäeva. Praegu toodetakse 170 000 m3 puitlaastplaati aastas

  4. Soome maiustustetootja Leaf saab peatselt uue omaniku / Tõnis Arnover

    Index Scriptorium Estoniae

    Arnover, Tõnis, 1952-

    2004-01-01

    Hollandi kontsern CSM otsustas loobuda maiustusetootmisest, sh. Soome magusatootjast Leaf ning keskenduda pagaritööstustoorme, biokemikaalide ning suhkrutoodete valmistamisele. Diagramm: CSMi kasumlikkus vähenes. Vt. samas: Eestis menukad kurgupastillid

  5. Kellest saab Alan Greenspani järeltulija? / Tõnis Oja

    Index Scriptorium Estoniae

    Oja, Tõnis, 1957-

    2005-01-01

    USA presidendil ei ole veel uut kandidaati ametist lahkuva keskpanga juhi Alan Greenspani asemele. Vt. samas: Alan Greenspani tegevuse olulisemad verstapostid keskpanga juhina; Pole välistatud ka ametikoha säilitamine

  6. Kui Kerry saab USA presidendiks, siis... / Anvar Samost

    Index Scriptorium Estoniae

    Samost, Anvar, 1971-

    2004-01-01

    Autor võrdleb USA presidendi George W. Bushi ja presidendikandidaat John Kerry välispoliitilisi seisukohti ning leiab, et peaaegu kõigis välispoliitika küsimustes on nad ühel meelel ja mõnes küsimuses on Kerry vaated pigem radikaalsemad

  7. Milline saab olema uuenenud WTO põllumajandusleping? / Ruve Schank

    Index Scriptorium Estoniae

    Šank, Ruve, 1954-

    2003-01-01

    Uuenenud WTO põllumajanduslepinguga hakkab riiklik toetus üha vähem olema seotud tootmisega, selle asemel toetatakse lihtsalt maal elamist ja seal töötamist põllumajandusega mitte otseselt seotud aladel

  8. Ülikooliga saab kohtuda ekraanil / Kerttu Jänese

    Index Scriptorium Estoniae

    Jänese, Kerttu, 1981-

    2007-01-01

    Tartu Ülikooli 375. aastapäeva puhul valminud dokumentaalfilm "Universitas Tartuensis 375" : stsenaristid Jaak Lõhmus ja Lauri Vahtre : režissöörid Rene Vilbre ja Märten Vaher : Estinfilm 2007. Filmist räägivad tegijad

  9. Aafrika saab endale esimese ühisarmee / Allan Espenberg

    Index Scriptorium Estoniae

    Espenberg, Allan

    2007-01-01

    Lõuna-Aafrika riikide majandusühenduse (Southern African Development Community) SADCi peaeesmärkidest ja tegevusest. Organisatsiooni 27. tippkohtumisel valiti uueks esimeheks Sambia president Levy Mwanawasa, samas otsustati moodustada ka regionaalne armee, mille peamiseks ülesandeks on rahumissioonide korraldamine ja elluviimine

  10. Ülesande lahendamise eest saab miljon dollarit / Harli Uljas

    Index Scriptorium Estoniae

    Uljas, Harli

    2000-01-01

    Maailma tippmatemaatikutele pakutakse seitset miljonit dollarit seitsme raske võrduse lahendamise eest. Clay Mathematics Institute pani probleemi üles oma internetileheküljele ja teatas sellest Pariisis toimunud konverentsil. Princetoni ülikooli matemaatikaprofessori Andrew Wilesi sõnul on need seitse matemaatilist probleemi selle ala kõige suuremad lahendamata väljakutsed

  11. Viru tunnel saab uue ilme urbanistliku grafiti abil / Ilmar Kahro

    Index Scriptorium Estoniae

    Kahro, Ilmar

    2011-01-01

    MTÜ Linnalabor koostöös Tallinn 2011 SA-ga viis läbi Tallinnas Gonsiori ja Laikmaa tänava ristmiku all paikneva Viru tunneli kujunduskonkursi "Viru tunnel kunstigaleriiks". EKA skulptuuri eriala tudengi Eldar Jakubovi võidutööst "Avame linna"

  12. Laenu tagamisest munitsipaalmaaga ehk kuidagi ikka saab / Rein Tiivel

    Index Scriptorium Estoniae

    Tiivel, Rein, 1940-

    2006-01-01

    AS Kinnisvaratehingud ja Puulinna Linnavalitsus leppisid kokku linna omandis oleva kinnisasja koormamises kinnisvarafirma kasuks. Esitatud kaasus sisaldas mitmeid kokkuleppeid, mis seadsid kahtluse alla tehingu kehtivuse ja valitud tee otstarbekuse

  13. Hea haridus saab alguse headest õpetajatest / Tõnis Lukas

    Index Scriptorium Estoniae

    Lukas, Tõnis, 1962-

    2008-01-01

    Ilmunud ka: Põhjarannik 2. veebr. 2008, lk. 4, Severnoje Poberezhje 2. veebr. 2008, lk. 4., Pärnu Postimees 2. veebr. lk 19, Meie Maa 4. veebr. lk. 2, Lääne Elu 5. veebr. 2008, lk. 2, Hiiu Leht 5. veebr. 2008, lk. 2, Nädaline 5. veebr. 2008, lk. 4., Võrumaa Teataja 5. veebr. lk. 2, Harju Elu 8. veebr. lk. 2, Koit 12. veebr. lk. 6, Järva Teataja 19. veebr. lk. 2, Sakala 20. veebr. lk. 2. Valitsus kiitis heaks haridusminister Tõnis Lukase poolt esitatud määruse eelnõu, mille kohaselt tõusevad õpetajate palkade alammäärad käesoleva aasta esimesest jaanuarist 22% võrra

  14. Kinnisvara pakkumishinda saab oluliselt alla kaubelda / Andres Hall

    Index Scriptorium Estoniae

    Hall, Andres

    2005-01-01

    Ilmunud ka: Molodjozh Estonii : Nedvizhimost 26. jaan. lk. 1, Delovõje Vedomosti 16. märts lk. 16. . Kinnisvara pakkumishinnad sisaldavad olulisel määral "õhku", mida ostjal on võimalik hinnast maha kaubelda

  15. Õunpuu saab Euroopa Talendi auhinna / Kristiina Davidjants

    Index Scriptorium Estoniae

    Davidjants, Kristiina, 1974-

    2008-01-01

    Cannes'i filmifestivali raames toimuval Euroopa päeval antakse filmirežissöör Veiko Õunpuule üle Euroopa Talendi auhind (European Talent Prize) mängufilmiprojekti "Püha Tõnu Kiusamine" eest (produtsent Katrin Kissa)

  16. Aero-acoustic Computations of Wind Turbines

    DEFF Research Database (Denmark)

    Shen, Wen Zhong; Michelsen, Jess; Sørensen, Jens Nørkær

    2002-01-01

    A numerical algorithm for acoustic noise generation is extended to 3D flows. The approach involves two parts comprising a viscous incompressible flow part and an inviscid acoustic part. In order to simulate noise generated from a wind turbine, the incompressible and acoustic equations are written...

  17. SAM2_AERO_PRF_NAT

    Data.gov (United States)

    National Aeronautics and Space Administration — Stratospheric Aerosol Measurement II - Aerosol Profile - Native format which measures solar irradiance attenuated by aerosol particles in the Arctic & Antarctic...

  18. The aero- and hydromechanics of keel yachts

    CERN Document Server

    Slooff, J W

    2015-01-01

    How and why does sail boat performance depend on the configuration and trim of boat and sails? This book provides the yachtsman with answers in a relatively straightforward account of the physical mechanisms of sailing. It presents an accessible overview of the fluid dynamic aspects of sailing and sailing technology, addressing both aeromechanics and hydromechanics.  Readers are provided with the basic principles of physics and general mechanics that will assist their understanding of the fluid mechanics of sailing yachts. Rich appendices cover not only in-depth, mathematical-physical treatments and derivations for those wishing to explore further, but also helpful summaries of basic mathematical notions for those wishing to refresh their knowledge.  This work explores keel yachts, specifically single-masted mono-hulls with ‘fore-and-aft’, Bermuda-rigged sails. However, much of it is applicable to other types of sailing vessels such as multi-hulls, yachts with multiple masts, windsurf boards and the li...

  19. Aero particles characterization emitted by mobile sources

    International Nuclear Information System (INIS)

    Rojas V, A.; Romero G, E. T.; Lopez G, H.

    2009-01-01

    In our country, the mobile sources that conform most of the emissions at the atmosphere, are concentrated on the urban areas. For the present work, samples coming from the escapes of terrestrial transport were obtained, such as: passenger buses, load transport and particular vehicles of the Metropolitan area of the Toluca valley. The material was analyzed by means of scanning electron microscopy of low vacuum and X-ray diffraction. The objective was to characterize the emitted particles by mobile sources, morphological and chemically to know the structure, size and elements that compose them. (Author)

  20. Aero-Acoustic Computations of Wind Turbines

    DEFF Research Database (Denmark)

    Zhu, Wei Jun

    2008-01-01

    both for laminar and turbulent flows. Results have shown that sound generation is due to the unsteadiness of the flow field and the spectrum of sound has a strong relation with fluctuating forces on the solid body. Flow and acoustic simulation were also carried out for a wind turbine where general...

  1. Aero-acoustic Computations of Wind Turbines

    DEFF Research Database (Denmark)

    Shen, Wen Zhong; Michelsen, Jess; Sørensen, Jens Nørkær

    2002-01-01

    A numerical algorithm for acoustic noise generation is extended to 3D flows. The approach involves two parts comprising a viscous incompressible flow part and an inviscid acoustic part. In order to simulate noise generated from a wind turbine, the incompressible and acoustic equations are written...... in polar coordinates. The developed algorithm is combined with a so-called actuator-line technique in which the loading is distributed along lines representing the blade forces. Computations are carried out for the 500kW Nordtank wind turbine equipped with three LM19 blades. ©2001 The American Institute...

  2. The DAN-AERO MW Experiments

    DEFF Research Database (Denmark)

    Aagaard Madsen, Helge; Bak, Christian; Schmidt Paulsen, Uwe

    a number of coordinated, innovative measurements on full scale MW size rotors as well as on airfoils for MW size turbines in wind tunnels. Shear and turbulence inflow characteristics were measured on a Siemens 3.6 MW turbine with a five hole pitot tube. Pressure and turbulent inflow characteristics were...... on the blade was further instrumented with around 50 microphones for high frequency surface pressure measurements. The surface pressure measurements have been correlated with inflow measurements from four five hole pitot tubes and two sensors for measuring the high frequency (50 Hz to10 kHz) contents...

  3. Aero-Hydroacoustics for Ships. Volume 1

    Science.gov (United States)

    1984-06-01

    be seen by evaluating the tangential gradient (l/r) 9p(rlc)/ 3d as = ’/2 and noting that it1" vanishes there. Thus we see that the normal velocity...W.H. and T. Roestel, "Berechnung der Druck -vCrteilun- and Flugeiprofilen in gashaltiger Wasscrstr6mun :," ZAI4M, Vol. 54, pp. 571-588 (197O4) S 3 S...Griffin and Ramberg measured greater vortex strengths with a peak-to-peak cyl- inder displacement of O. 3d than with no motion. This increase in circulation

  4. Fluid Temperature of Aero Hydraulic Systems

    Directory of Open Access Journals (Sweden)

    I. S. Shumilov

    2016-01-01

    Full Text Available In modern supersonic aircrafts due to aerodynamic skin heating a temperature of hydraulics environment significantly exceeds that of permissible for fluids used. The same problem exists for subsonic passenger aircrafts, especially for Airbuses, which have hydraulics of high power where convective heat transfer with the environment is insufficient and there is no required temperature control of fluid. The most significant in terms of heat flow is the flow caused by the loss of power to the pump and when designing the hydraulic system (HS it is necessary to pay very serious attention to it. To use a constant capacity pump is absolutely unacceptable, since HS efficiency in this case is extremely low, and the most appropriate are variable-capacity pumps, cut-off pumps, dual-mode pumps. The HS fluid cooling system should provide high reliability, lightweight, simple design, and a specified heat transfer in all flight modes.A system cooling the fluid by the fuel of feeding lines of the aircraft engines is the most effective, and it is widely used in supersonic aircrafts, where power of cooling system is essential. Subsonic aircrafts widely use convective heat exchangers. In thermal design of the aircraft hydraulics, the focus is generally given to the maximum and minimum temperatures of the HS fluid, the choice of the type of heat exchanger (convective or flow-through, the place of its installation. In calculating the operating temperature of a hydraulic system and its cooling systems it is necessary to determine an increase of the working fluid temperature when throttling it. There are three possible formulas to calculate the fluid temperature in throttling, with the error of a calculated temperature drop from 30% to 4%.The article considers the HS stationary and noon-stationary operating conditions and their calculation, defines temperatures of fluid and methods to control its specified temperature. It also discusses various heat exchanger schemes, makes recommendations for regulation of heat flows, power reduction of cooling system, and choice of heat insulation elements of HS.

  5. Cleaner aero-engines taking off

    International Nuclear Information System (INIS)

    Lothigius, J.

    1991-01-01

    Airlines operating on domestic routes in Sweden have to pay taxes on their emissions of nitrogen oxides, hydrocarbons and carbon dioxide. These taxes have spurred improvements in engine design, but are unlikely to slow the growth in air traffic

  6. Aero-acoustic performance of Fractal Spoilers

    Science.gov (United States)

    Nedic, J.; Ganapathisubramani, B.; Vassilicos, C.; Boree, J.; Brizzi, L.; Spohn, A.

    2010-11-01

    One of the major environmental problems facing the aviation industry is that of aircraft noise. The work presented in this paper, done as part of the OPENAIR Project, looks at reducing spoiler noise through means of large-scale fractal porosity. It is hypothesised that the highly turbulent flow generated by these grids, which have multi-length-scales, would remove the re-circulation region and with it, the low frequency noise it generates. In its place, a higher frequency noise is introduced which is susceptible to atmospheric attenuation, and would be deemed less offensive to the human ear. A total of nine laboratory scaled spoilers were looked at, seven of which had a fractal design, one conventionally porous and one solid for reference. All of the spoilers were mounted on a flat plate and inclined at 30^o to the horizontal. Far-field, microphone array and PIV measurements were taken in an anechoic chamber to determine the acoustic performance and to study the flow coming through the spoilers. A significant reduction in sound pressure level is recorded and is found to be very sensitive to small changes in fractal grid parameters. Wake and drag force measurements indicated that the spoilers increase the drag whilst having minimal effect on the lift.

  7. Theoretical and experimental study of heat transfers and pressure drops along surfaces fitted with herring-bone fins: correlation between geometric and aero thermal parameters; Etudes theorique et experimentale du transfert de chaleur et des pertes de charge de surfaces munies d'ailettes disposees en chevron - correlation entre parametres geometriques et aerothermiques

    Energy Technology Data Exchange (ETDEWEB)

    Pelce, J; Malherbe, J; Pierre, B [Commissariat a l' Energie Atomique, Saclay (France). Centre d' Etudes Nucleaires

    1965-07-01

    Principal results are given of experimental research which has been carried out on the flow of a fluid along a surface fitted with herringbone fins. Aero-thermal tests have been effected on a large number of these surfaces whose geometrical parameters have been made to vary systematically. In particular, work on a large scale model has made it possible to analyse the mechanisms of heat transfer and of pressure drops. On this basis a theoretical study has led to the establishment of a correlation between the geometric configuration and the aero-thermal performances of these surfaces. Experimental results are in good agreement with the theoretical relationships. An expression has thus been derived applicable to this type of herring-boned surface in a wide zone. (authors) [French] L'ecoulement d'un fluide au voisinage d'une surface munie d'ailettes disposees en chevron a fait l'objet de recherches experimentales dont on a rappele les principaux resultats. Des essais aerothermiques ont ete effectues sur un grand nombre de ces surfaces dont a fait varier les parametres geometriques de facon systematique. En particulier, des etudes sur une maquette a grande echelle ont permis d'analyser les mecanismes de transfert de chaleur et de perte de charge. Sur ces bases, une etude theorique a conduit a des correlations entre la geometrie et les performances aerothermiques de ces surfaces. Les resultats experimentaux sont en bon accord avec les relations theoriques. On possede ainsi une formulation pour ce type de surface ailettee valable dans un domaine etendu. (auteurs)

  8. 49 CFR Appendix A-I to Part 541 - Lines With Antitheft Devices Which Are Exempted From the Parts-Marking Requirements of This...

    Science.gov (United States)

    2010-10-01

    .... Outlander.1 Nissan Altima. Cube.1 Maxima. Murano. Pathfinder. Quest. Rogue. Sentra. Versa. Infiniti G.2 Infiniti M.3 Porsche 911. Boxster/Cayman. Panamera. Saab 9-3. 9-5.1 Subaru Forester. Impreza. Legacy.1 B9.... Tiguan.1 1 Granted an exemption from the parts marking requirements beginning with MY 2011. 2 Infiniti G...

  9. Autolehe kõige põhjalikum autotest

    Index Scriptorium Estoniae

    2011-01-01

    10 toimetuse sõiduki pikaaegne kasutustest: BMW R1100S (1999), Chrysler Sebring (2002), Dacia Duster (2011), Ford Sierra (1983), Mercedes-Benz 500 SEL (1990), Mitsubishi Galant (1989), Saab 9-5 (1999), Subaru Legacy (2007), Škoda Fabia RS (2010) ja Toyota MR 2 (1988)

  10. Revised physical elements of the astrophysically important O9.5+O9.5V eclipsing binary system Y Cygni

    Czech Academy of Sciences Publication Activity Database

    Harmanec, P.; Holmgren, D. E.; Wolf, M.; Božić, H.; Guinan, E. F.; Kang, Y. W.; Mayer, P.; McCook, G.; Nemravová, J.; Yang, S.; Šlechta, Miroslav; Ruzdjak, D.; Sudar, D.; Svoboda, P.

    2014-01-01

    Roč. 563, March (2014), A120/1-A120/12 ISSN 0004-6361 R&D Projects: GA ČR GA205/06/0584 Institutional research plan: CEZ:AV0Z10030501 Keywords : binaries: spectroscopic * stars: fundamental parameters Subject RIV: BN - Astronomy, Celestial Mechanics, Astrophysics Impact factor: 4.378, year: 2014

  11. 26 CFR 1.401(a)(9)-5 - Required minimum distributions from defined contribution plans.

    Science.gov (United States)

    2010-04-01

    ... OF THE TREASURY (CONTINUED) INCOME TAX (CONTINUED) INCOME TAXES Pension, Profit-Sharing, Stock Bonus... by the purchase of an annuity contract from an insurance company in accordance with A-4 of § 1.401(a... invested only in productive assets. A named a testamentary trust (Trust P) established under A's will as...

  12. 28 CFR 9.5 - Criteria governing administrative and judicial remission and mitigation.

    Science.gov (United States)

    2010-07-01

    ... property was subject to forfeiture at the time of the purchase, or is one who held a legally cognizable... the offense underlying the forfeiture where certain mitigating factors exist, including, but not... petitioner fails to accept the Ruling Official's mitigation decision or any of its conditions, or fails to...

  13. Solar-like oscillations in the G9.5 subgiant β Aquilae

    DEFF Research Database (Denmark)

    Corsaro, E.; Grundahl, F.; Leccia, S.

    2012-01-01

    was observed during six nights in August 2009 by means of the high-resolution \\'echelle spectrograph SARG operating with the TNG 3.58 m Italian telescope on the Canary Islands, exploiting the iodine cell technique. We present the result and the detailed analysis of high-precision radial velocity measurements...

  14. Development of a pulsed 9.5 micron lidar for regional scale O3 measurement

    Science.gov (United States)

    Stewart, R. W.

    1980-01-01

    A pulsed infrared lidar system designed for application to the remote sensing of atmospheric trace gases from an airborne platform is described. The system is also capable of measuring the infrared backscatter characteristics of the ocean surface, terrain, cloud, and aerosol targets. The lidar employed is based on dual wavelength pulse energy measurements in the 9-11 micrometer wavelength region.

  15. Advanced materials and protective coatings in aero-engines application

    OpenAIRE

    M. Hetmańczyk; L. Swadźba; B. Mendala

    2007-01-01

    Purpose: The following article demonstrates the characteristics of the materials applied as parts of aircraft engine turbines and the stationary gas turbines. The principal technologies for manufacturing the heat resistant coatings and the erosion and corrosion resistant coatings were characterized. Sample applications for the aforementioned coatings are presented: on turbine blades, compressor blades and on parts of combustion chambers of aircraft engines.Design/methodology/approach: The nic...

  16. Combined Aero and Underhood Thermal Analysis for Heavy Duty Trucks

    Energy Technology Data Exchange (ETDEWEB)

    Vegendla, Prasad [Argonne National Lab. (ANL), Argonne, IL (United States); Sofu, Tanju [Argonne National Lab. (ANL), Argonne, IL (United States); Saha, Rohit [Cummins Inc., Columbus, IN (United States); Madurai Kumar, Mahesh [Cummins Inc., Columbus, IN (United States); Hwang, L. K [Cummins Inc., Columbus, IN (United States)

    2017-01-31

    Aerodynamic analysis of the medium-duty delivery truck was performed to achieve vehicle design optimization. Three dimensional CFD simulations were carried out for several improved designs, with a detailed external component analysis of wheel covers, side skirts, roof fairings, and rounded trailer corners. The overall averaged aerodynamics drag reduction through the design modifications were shown up to 22.3% through aerodynamic considerations alone, which is equivalent to 11.16% fuel savings. The main identified fuel efficiencies were based on second generation devices, including wheel covers, side skirts, roof fairings, and rounded trailer corners. The important findings of this work were; (i) the optimum curvature radius of the rounded trailer edges found to be 125 mm, with an arc length of 196.3 mm, (ii) aerodynamic drag reduction increases with dropping clearance of side skirts between wheels and ground, and (iii) aerodynamic drag reduction increases with an extension of front bumper towards the ground.

  17. Process Improvement Through Tool Integration in Aero-Mechanical Design

    Science.gov (United States)

    Briggs, Clark

    2010-01-01

    Emerging capabilities in commercial design tools promise to significantly improve the multi-disciplinary and inter-disciplinary design and analysis coverage for aerospace mechanical engineers. This paper explores the analysis process for two example problems of a wing and flap mechanical drive system and an aircraft landing gear door panel. The examples begin with the design solid models and include various analysis disciplines such as structural stress and aerodynamic loads. Analytical methods include CFD, multi-body dynamics with flexible bodies and structural analysis. Elements of analysis data management, data visualization and collaboration are also included.

  18. Micro-Optical Distributed Sensors for Aero Propulsion Applications

    Science.gov (United States)

    Arnold, S.; Otugen, V.

    2003-01-01

    The objective of this research is to develop micro-opto-mechanical system (MOMS)-based sensors for time- and space-resolved measurements of flow properties in aerodynamics applications. The measurement technique we propose uses optical resonances in dielectric micro-spheres that can be excited by radiation tunneling from optical fibers. It exploits the tunneling-induced and morphology-dependent shifts in the resonant frequencies. The shift in the resonant frequency is dependent on the size, shape, and index of refraction of the micro-sphere. A physical change in the environment surrounding a micro-bead can change one or more of these properties of the sphere thereby causing a shift in frequency of resonance. The change of the resonance frequency can be detected with high resolution by scanning a frequency-tunable laser that is coupled into the fiber and observing the transmission spectrum at the output of the fiber. It is expected that, in the future, the measurement concept will lead to a system of distributed micro-sensors providing spatial data resolved in time and space. The present project focuses on the development and demonstration of temperature sensors using the morphology-dependent optical resonances although in the latter part of the work, we will also develop a pressure sensor. During the period covered in this report, the optical and electronic equipment necessary for the experimental work was assembled and the experimental setup was designed for the single sensor temperature measurements. Software was developed for real-time tracking of the optical resonance shifts. Some preliminary experiments were also carried out to detect temperature using a single bead in a water bath.

  19. Denutrition et cancers des voies aero-digestives superieures ...

    African Journals Online (AJOL)

    Head and neck cancer and its treatment are responsible in more than 30% of cases of malnutrition witch can be severe and interfere with the management of these tumors. The aim of this paper is to provide a protocol for nutritional management practices of these cancers. The malnutrition diagnosis requires an examination ...

  20. Aero-Mechanical Coupling in a High-Speed Compressor

    Science.gov (United States)

    2010-02-01

    freedom mass-spring- damper system as χ = ς 2 √ κµ . (51) ς represents the viscous damping, κ is the system stiffness and µ the system mass. χ expresses...between the fluid and structures which are common in modern, high-speed axial compressors. There were two major areas of focus. The first was the...development of measurement technique specifically for the study of these phenomena, termed Blade Image Velocimetry (BIV). The technique can measure fluid and

  1. Reflexive Aero Structures for Enhanced Survivability, Phase II

    Data.gov (United States)

    National Aeronautics and Space Administration — Cornerstone Research Group Inc. (CRG) will develop an advanced reflexive structure technology system to increase the survivability of future systems constructed of...

  2. Aero-Acoustic-Structural Optimization Analysis and Testing, Phase I

    Data.gov (United States)

    National Aeronautics and Space Administration — This proposal effort is concerned with the development of a novel multidisciplinary optimization scheme and computer software for the effective design of advanced...

  3. Performance optimization of grooved slippers for aero hydraulic pumps

    Directory of Open Access Journals (Sweden)

    Juan Chen

    2016-06-01

    Full Text Available A computational fluid dynamics (CFD simulation method based on 3-D Navier–Stokes equation and Arbitrary Lagrangian–Eulerian (ALE method is presented to analyze the grooved slipper performance of piston pump. The moving domain of grooved slipper is transformed into a fixed reference domain by the ALE method, which makes it convenient to take the effects of rotate speed, body force, temperature, and oil viscosity into account. A geometric model to express the complex structure, which covers the orifice of piston and slipper, vented groove and the oil film, is constructed. Corresponding to different oil film thicknesses calculated in light of hydrostatic equilibrium theory and boundary conditions, a set of simulations is conducted in COMSOL to analyze the pump characteristics and effects of geometry (groove width and radius, orifice size on these characteristics. Furthermore, the mechanics and hydraulics analyses are employed to validate the CFD model, and there is an excellent agreement between simulation and analytical results. The simulation results show that the sealing land radius, orifice size and groove width all dramatically affect the slipper behavior, and an optimum tradeoff among these factors is conducive to optimizing the pump design.

  4. Aero-Elastic Optimization of a 10 MW Wind Turbine

    DEFF Research Database (Denmark)

    Zahle, Frederik; Tibaldi, Carlo; Verelst, David Robert

    2015-01-01

    This article describes a multi-disciplinary optimization and analysis tool for wind turbines that is based on the open-source framework OpenMDAO. Interfaces to several simulation codes have been implemented which allows for a wide variety of problem formulations and combinations of models....... In this article concurrent aeroelastic optimization of a 10 MW wind turbine rotor is carried out with respect to material distribution distribution and planform. The optimizations achieve up to 13% mass reduction while maintaining the same power production compared to the baseline DTU 10MW RWT....

  5. Control of Boundary Layers for Aero-optical Applications

    Science.gov (United States)

    2015-06-23

    with some difficulty) from hot-wire velocity measurements, or computed directly from CFD results (e.g. Wang & Wang, 2012). Several different density...of experimental and computational research, especially applied to supersonic and hypersonic boundary layers; see Smits & Dussauge (1996), Spina et...Duan, L., Beekman, I. and Martin, M.P. (2010) Direct Numerical Simulation of Hypersonic Turbulent Boundary Layers. Part 2. Effect of Wall

  6. Hypersonic CFD applications for the National Aero-Space Plane

    Science.gov (United States)

    Richardson, Pamela F.; Mcclinton, Charles R.; Bittner, Robert D.; Dilley, A. Douglas; Edwards, Kelvin W.

    1989-01-01

    Design and analysis of the NASP depends heavily upon developing the critical technology areas that cover the entire engineering design of the vehicle. These areas include materials, structures, propulsion systems, propellants, integration of airframe and propulsion systems, controls, subsystems, and aerodynamics areas. Currently, verification of many of the classical engineering tools relies heavily on computational fluid dynamics. Advances are being made in the development of CFD codes to accomplish nose-to-tail analyses for hypersonic aircraft. Additional details involving the partial development, analysis, verification, and application of the CFL3D code and the SPARK combustor code are discussed. A nonequilibrium version of CFL3D that is presently being developed and tested is also described. Examples are given of portion calculations for research hypersonic aircraft geometries and comparisons with experiment data show good agreement.

  7. Assessment of Aero-radiometric Data of Southern Anambra Basin ...

    African Journals Online (AJOL)

    ADOWIE PERE

    Potassium and Thorium) were used and processed independently to investigate the Southern. Anambra basin for the .... Based on the Rybach equation (1) above, Uranium produces the .... Geothermal Exploration: State of the Art. Techniques.

  8. Receding-horizon adaptive contyrol of aero-optical wavefronts

    NARCIS (Netherlands)

    Tesch, J.; Gibson, S.; Verhaegen, M.

    2013-01-01

    A new method for adaptive prediction and correction of wavefront errors in adaptive optics (AO) is introduced. The new method is based on receding-horizon control design and an adaptive lattice filter. Experimental results presented illustrate the capability of the new adaptive controller to predict

  9. Reflexive Aero Structures for Enhanced Survivability, Phase I

    Data.gov (United States)

    National Aeronautics and Space Administration — Cornerstone Research Group Inc. (CRG) proposes to develop an advanced reflexive structure system to increase the survivability of aerostructures. This reflexive...

  10. Overview of NASA Glenn Aero/Mobile Communications Demonstrations

    Science.gov (United States)

    Brooks, David; Hoder, Doug; Wilkins, Ryan

    2004-01-01

    The Glenn Research Center at Lewis Field (GRC) has been involved with several other NASA field centers on various networking and RF communications demonstrations and experiments since 1998. These collaborative experiments investigated communications technologies new to aviation, such as wideband Ku satcom, L-band narrowband satcom, and IP (Internet Protocol), using commercial off-the-shelf (COTS) components These technologies can be used to distribute weather and hazard data, air traffic management and airline fleet management information, and passenger cabin Internet service.

  11. Overview of NASA Glenn Aero/Mobile Communication Demonstrations

    Science.gov (United States)

    Brooks, David; Hoder, Doug; Wilkins, Ryan

    2004-01-01

    The Glenn Research Center at Lewis Field (GRC) has been involved with several other NASA field centers on various networking and RF communications demonstrations and experiments since 1998. These collaborative experiments investigated communications technologies new to aviation, such as wideband Ku satcom, L-band narrowband satcom, and IP (Internet Protocol), using commercial off-the-shelf (COTS) components These technologies can be used to distribute weather and hazard data, air traffic management and airline fleet management information, and passenger cabin Internet service.

  12. Dynamic Systems Analysis for Turbine Based Aero Propulsion Systems

    Science.gov (United States)

    Csank, Jeffrey T.

    2016-01-01

    The aircraft engine design process seeks to optimize the overall system-level performance, weight, and cost for a given concept. Steady-state simulations and data are used to identify trade-offs that should be balanced to optimize the system in a process known as systems analysis. These systems analysis simulations and data may not adequately capture the true performance trade-offs that exist during transient operation. Dynamic systems analysis provides the capability for assessing the dynamic tradeoffs at an earlier stage of the engine design process. The dynamic systems analysis concept, developed tools, and potential benefit are presented in this paper. To provide this capability, the Tool for Turbine Engine Closed-loop Transient Analysis (TTECTrA) was developed to provide the user with an estimate of the closed-loop performance (response time) and operability (high pressure compressor surge margin) for a given engine design and set of control design requirements. TTECTrA along with engine deterioration information, can be used to develop a more generic relationship between performance and operability that can impact the engine design constraints and potentially lead to a more efficient engine.

  13. Aero dynamical and mechanical behaviour of the Savonius rotor

    Energy Technology Data Exchange (ETDEWEB)

    Aouachria, Z. [Batna Univ., (Algeria). Applied Energetic Physics Laboratory

    2009-07-01

    Although the Savonius wind turbine is not as efficient as the traditional Darrieus wind turbine, its rotor design has many advantages such as simple construction; acceptance of wind from all directions; high starting torque; operation at relatively low speed; and easy adaptation to urban sites. These advantages may outweigh its low efficiency and make it suitable for small-scale power requirements such as pumping and rural electrification. This paper presented a study of the aerodynamic behaviour of a Savonius rotor, based on blade pressure measurements. A two-dimensional analysis method was used to determine the aerodynamic strengths, which leads to the Magnus effect and the generation of the vibrations on the rotor. The study explained the vibratory behaviour of the rotor and proposed an antivibration system to protect the machine. 14 refs., 1 tab., 9 figs.

  14. Multidisciplinary Aerospace Systems Optimization: Computational AeroSciences (CAS) Project

    Science.gov (United States)

    Kodiyalam, S.; Sobieski, Jaroslaw S. (Technical Monitor)

    2001-01-01

    The report describes a method for performing optimization of a system whose analysis is so expensive that it is impractical to let the optimization code invoke it directly because excessive computational cost and elapsed time might result. In such situation it is imperative to have user control the number of times the analysis is invoked. The reported method achieves that by two techniques in the Design of Experiment category: a uniform dispersal of the trial design points over a n-dimensional hypersphere and a response surface fitting, and the technique of krigging. Analyses of all the trial designs whose number may be set by the user are performed before activation of the optimization code and the results are stored as a data base. That code is then executed and referred to the above data base. Two applications, one of the airborne laser system, and one of an aircraft optimization illustrate the method application.

  15. Airborne Aero-Optics Laboratory - Transonic (AAOL-T)

    Science.gov (United States)

    2016-10-03

    the complexity of the turret wake are displayed in Figure 33. Figure 33. Visualizations of lambda 2 (vortex identification method), fluctuating...wavefront, the POD modes must span the entire set if the training matrix is full rank. In general, this will be true for experimental data, although the...highest-order modes are likely contaminated with noise. Thus, the value for N will be equal to the number of subapertures in the wavefront matrix for a

  16. Aero-Heating of Shallow Cavities in Hypersonic Freestream Flow

    Science.gov (United States)

    Everhart, Joel L.; Berger, Karen T.; Merski, N. R., Jr.; Woods, William A.; Hollingsworth, Kevin E.; Hyatt, Andrew; Prabhu, Ramadas K.

    2010-01-01

    The purpose of these experiments and analysis was to augment the heating database and tools used for assessment of impact-induced shallow-cavity damage to the thermal protection system of the Space Shuttle Orbiter. The effect of length and depth on the local heating disturbance of rectangular cavities tested at hypersonic freestream conditions has been globally assessed using the two-color phosphor thermography method. These rapid-response experiments were conducted in the Langley 31-Inch Mach 10 Tunnel and were initiated immediately prior to the launch of STS-114, the initial flight in the Space Shuttle Return-To-Flight Program, and continued during the first week of the mission. Previously-designed and numerically-characterized blunted-nose baseline flat plates were used as the test surfaces. Three-dimensional computational predictions of the entire model geometry were used as a check on the design process and the two-dimensional flow assumptions used for the data analysis. The experimental boundary layer state conditions were inferred using the measured heating distributions on a no-cavity test article. Two test plates were developed, each containing 4 equally-spaced spanwise-distributed cavities. The first test plate contained cavities with a constant length-to-depth ratio of 8 with design point depth-to-boundary-layer-thickness ratios of 0.1, 0.2, 0.35, and 0.5. The second test plate contained cavities with a constant design point depth-to-boundary-layer-thickness ratio of 0.35 with length-to-depth ratios of 8, 12, 16, and 20. Cavity design parameters and the test condition matrix were established using the computational predictions. Preliminary results indicate that the floor-averaged Bump Factor (local heating rate nondimensionalized by upstream reference) at the tested conditions is approximately 0.3 with a standard deviation of 0.04 for laminar-in/laminar-out conditions when the cavity length-to-boundary-layer thickness is between 2.5 and 10 and for cavities in the depth-to-boundary-layer-thickness range of 0.3 to 0.8. Over this same range of conditions and parameters, preliminary results also indicate that the maximum Bump Factor on the cavity centerline falls between 2.0 and 2.75, as long as the cavity-exit conditions remain laminar. Cavities with length-to-boundary-layer-thickness ratio less than 2.5 can not be easily classified with this approach and require further analysis.

  17. Kuidas kantslerist saab euroametnik: Matti Maasika lugu / Matti Maasikas ; intervjueerinud Erkki Bahovski

    Index Scriptorium Estoniae

    Maasikas, Matti

    2009-01-01

    Välisministeeriumi kantsleri kohalt Brüsselisse Euroopa Komisjoni laienemisvoliniku Olli Rahni kabinetti tööle asunud Matti Maasikas vastab küsimustele, mis puudutavad uuele töökohale asumist, tööülesandeid ning Albaania, Makedoonia ja Montenegro liitumist Euroopa Liiduga. Vt. samas: Lühike ametikäik

  18. Sponsorlus - kas kasu saab aidatav või aitaja? / Heie Treier

    Index Scriptorium Estoniae

    Treier, Heie, 1963-

    1998-01-01

    Raamatust "Mõtete vabakaubandus", milles vestlevad saksa päritolu ameerika kunstnik Hans Haacke ning prantsuse filosoof ja sotsioloog Pierre Bourdieu kultuuri rahastamisest. Helsingis juunis Kiasma korraldatud samateemalisest seminarist. Kurioosumeid Eestist

  19. Ruhnu sadama sissesõidutee saab lõpuks ohutuma märgistuse

    Index Scriptorium Estoniae

    2009-01-01

    Ruhnu piirivalvekordoni ülem Rainer Sosi pöördus veeteede ameti poole, et viimane paigaldaks õnnetuste ärahoidmiseks Ruhnu saare lähedale nn Ringsu rabasse korraliku poi. Aastate jooksul on selles paigas mitmeid aluseid karile sõitnud

  20. Plektrumil saab MediaLabis digikunstniku tööd proovida / Anne Vetik

    Index Scriptorium Estoniae

    Vetik, Anne

    2006-01-01

    Eesti Meediakunstnike Ühingu ja Kultuuritehase Polymer koostöös sündinud "MediaLab Tallinn" Madara 22 tutvustab ennast 15.-19. nov. 2006. a. visuaalsete helide festivalil Plektrum. Piibe Piirma ja Marge Paasi sõnul piiritlevad nad oma tegevust sõnadega "digitaalne kunst"

  1. Investor saab majandustsükli faase ära kasutada / Romet Kreek

    Index Scriptorium Estoniae

    Kreek, Romet, 1972-

    2005-01-01

    Majandustsükli erinevate faaside jooksul kipuvad erinevate sektorite aktsiad erinevalt käituma ja seda püütakse ära kasutada, roteerides rahapaigutusi erinevate sektorite aktsiatesse või indeksiaktsiatesse

  2. Eduka ettevõtte aluseks saab olla vaid looming / Ave Schmidt

    Index Scriptorium Estoniae

    Schmidt, Ave

    2010-01-01

    Tänapäeva ettevõttele tagavad konkurentsieelise inspiratsioon ja originaalsed ideed. Arvamust avaldavad Tallinna kohviku Nop asutaja Margit Aasmäe, Estonian Airi arendusdirektor Gunnar Mägi, Tallinna Kaubamaja müügi- ja turundusdirektor Enn Parel ja Balteco disainijuht Aivar Habakukk

  3. Eestlane saab tööd ka Mustal Mandril / Reelika Võsang

    Index Scriptorium Estoniae

    Võsang, Reelika

    2005-01-01

    Heategevusorganisatsiooni Humana People to People projektidega on võimalik liituda igaühel, kes ei karda väljakutseid, pingelist koolitust ja tööd ning soovib teisi aidata. Samas räägib vabatahtliku elust Aafrikas Jana Teppih. Lisa: Fakte aidsist

  4. Oma ala meistriks saab igaüks isemoodi / Anna-Liisa Mets

    Index Scriptorium Estoniae

    Mets, Anna-Liisa

    2014-01-01

    Selgusid kutsemeistrivõistluse "Noor meister 2014" parimad. Edukalt esinenud õppurid meisterkondiiter Helen Laht, ehituspuussepp Mirko Pruus, logistik Karl-Erik Maripuu, keskkonnatehnika lukksepp Robert Born, elektrik Tiit Talts ja müürsepp Sander Hindrikus räägivad oma ametiõpingutest ja tulevikuplaanidest

  5. Unes saab mitut moodi kõndida / Lauri Kärk

    Index Scriptorium Estoniae

    Kärk, Lauri, 1954-

    2002-01-01

    Pimedate Ööde Filmifestivali raames toimuva tudengifilmide festivali programmist "Vanad ja väärikad", kus näidati maailmakuulsate režissööride esimesi katsetusi ning kuulsate eksperimentaalfilmide autorite underground-filmide kavast

  6. Raskustes Onistari tennisehall saab rahasüsti / Toivo Tänavsuu

    Index Scriptorium Estoniae

    Tänavsuu, Toivo

    2005-01-01

    Rootsi investeerimisfondide haldusfirma Askembla Asset Management investeerib Onistari tennisehalli 20 miljonit krooni, kuhu rajab veekompleksi ja Eesti ühe suurema jõusaali. Lisa: Konkurent: julge ettevõtmine

  7. Papp-prillid pähe : täna õhtul saab stereokino / Maris Meiessaar

    Index Scriptorium Estoniae

    Meiessaar, Maris

    2008-01-01

    Animafilmide festivali "Animated Dreams" loenguprogrammis Keyframes esineb täna Von Krahli teatris hollandi stereofilmi guru Alexander Lentjes. Filmide osas näeb ka Andres Tenusaare uut stereofilmi "Miriami piknik"

  8. Ettevõtja saab maaostuks laenu / Silja Lättemäe

    Index Scriptorium Estoniae

    Lättemäe, Silja, 1952-

    2004-01-01

    Maaelu Edendamise Sihtasutus annab maaostuks laenu 25 aastaks intressiga 6% aastas. Tabel: Kutsekoolidele jagatavad MES-i stipendiumid. Vt. ka: Kuidas hindate MESi tööd? Küsimusele vastab Eesti Põllumajandus-Kaubanduskoja juhatuse esimees Ester Tuiksoo

  9. Väikeste sammudega saab jõudsamalt edasi liikuda / Liisi Seil

    Index Scriptorium Estoniae

    Seil, Liisi, 1971-

    2009-01-01

    Täiskasvanud õppija nädala raames tunnustati Viljandimaa aasta parimaid. Aasta õppija tiitli pälvis OÜ Sveba-Dahlen tootmistehnik Raul Järve, aasta koolitaja on vabakutseline õpetaja Enn Onni ning aasta koolitussõbralikemaks omavalitsuseks tunnistati Tarvastu Vallavalitsus

  10. Pedagoogikaülikoolis saab õppida eurotõlgiks / Helve Laasik

    Index Scriptorium Estoniae

    Laasik, Helve, 1958-

    2002-01-01

    2002. a. avas Tallinna Pedagoogikaülikool tõlkide magistriõppe, konkurss oli suur. Magistriõpe kestab kaks aastat, esimene semester on sissejuhatav, teisest semestrist lähevad suuliste ja kirjalike tõlkide õppekavad lahku

  11. Endine linnaametnik saab pealinna suurpargi golfiväljakute rajamiseks / Silva Männik

    Index Scriptorium Estoniae

    Männik, Silva, 1974-

    2004-01-01

    Endise linnaametniku Tarmo Valgepea poolt juhitav MTÜ Eesti Golfi Liit sai Pirital asuva ligi 30 ha suuruse Lillepi pargi hoonestusõiguse sotsiaalmaa maksustamise hinnaga. Kaart: Tallinna suuruselt teine park muutub golfikeskuseks

  12. Maailma farmaatsiatööstus saab Tartust topeltkiirenduse / Nils Niitra

    Index Scriptorium Estoniae

    Niitra, Nils, 1975-

    2004-01-01

    Tänavu sügisel valmib Tartu Ülikoolis Euroopa Liidu rahastatud molekulaardisaini süsteem, mis kahandab uute ravimite väljatöötamise kestust maailmas seniselt 15 aastalt 7-8 aastani. Lisad: Mis on molekulaardisain?, Mis on grid? Vt. ka Postimehes pealk. all: Tartu Ülikool aitab ravimitootjaid

  13. Kolmanda põlvkonna mobiilside saab hoogu / Tõnu Grünberg

    Index Scriptorium Estoniae

    Grünberg, Tõnu, 1963-

    2003-01-01

    EMT arendus- ja tehnoloogiadirektor Tõnu Grünberg kommenteerib 3G mobiilsidevõrgu arengut maailmas ning prognoosib, et aastaks 2005 jõutakse ka Eestis toimiva 3G kommertsvõrguni. 3G toob mobiilse andmeside arengusse olulise hüppe, leiab autor

  14. Raikülast saab Eesti mõisate süda / Imbi Raikna

    Index Scriptorium Estoniae

    Raikna, Imbi

    2004-01-01

    Raikküla mõisa ajaloost, omanikest. Mõisahoone arhitektiks arvatakse olevat Johann Carl Ludwig Engel. Raikküla mõisa tegi kuulsaks Keyserlingide suguvõsa. 1999. a. omandas mõisa perekond Jõesoo, kes on hüljatud valduse ellu äratanud, kavandades sinna raamatumõisa ja mõisainfo keskust. 10 ill

  15. Toetusi saab küsida ka LEADER-programmi raames / Raavo Raadik

    Index Scriptorium Estoniae

    Raadik, Raavo

    2011-01-01

    Eesti Hobusekasvatajate Seltsi raskeveohobuse kasvatajate haruseltsi juht Enn Rand on LEADER-programmi abil oluliselt arendanud Pärnumaal Tõstamaa vallas asuvat Maria talu, mis on praeguseks muutunud maakonnas arvestatavaks puhke- ja spordikeskuseks

  16. Puhkusereisist saab ohtlik seiklus. Kas reisija või reisikorraldaja risk? / Maria Pihlak, Urmas Volens

    Index Scriptorium Estoniae

    Pihlak, Maria, 1988-

    2017-01-01

    Reisi ohtlikuks muutumisega seonduvast riskijaotusest võlaõigusseaduse alusel ja asjakohasest kohtupraktikast. Reisikorraldaja teavitamiskohustusest ja pakettreisilepingu ülesütlemisest vääramatu jõu tõttu

  17. Vanilla Ninjast saab vene bänd / Viktoria Ladõnskaja

    Index Scriptorium Estoniae

    Ladõnskaja, Viktoria, 1981-

    2007-01-01

    Plaadifirmalt Topten Vanilla Ninja lepingu ära ostnud jurist Aleksander Simakov kuulutab välja konkursi bändi uute tüdrukute leidmiseks, bänd koosseisus Piret Järvis, Lenna Kuurmaa ja Katrin Siska kavatsevad ka Vanilla Ninja nime all jätkata

  18. FSB : terror saab tuge välismaa MTÜdelt / Oliver Tiks

    Index Scriptorium Estoniae

    Tiks, Oliver

    2008-01-01

    Venemaa föderaalse julgeolekuteenistuse FSB peadirektor Nikolai Patrushev süüdistab välismaiseid valitsusväliseid organisatsioone rahvusvaheliste terroristide aitamises, värvates terroristide toetajaid Venemaa territooriumil

  19. Lembit Peterson: teatris saab tegelda südametunnistuse äratamisega / intervjueerinud Andres Laasik

    Index Scriptorium Estoniae

    Peterson, Lembit, 1953-

    2011-01-01

    Tahkuna tuletornis septembris esietendunud lavastusest "Üks suvepäev", mis jõudis Theatrumi teatrisaali. Näidendi autorist Jon Fossest. Sellest, kuidas tekkis mõte mängida etendust Tahkuna tuletornis. Lavastusest "Misantroop", mida etendatakse Kadrioru lossis. Theatrumi publikust, suhtlemisest publikuga, majanduslikust olukorrast

  20. Kas Euroopast saab maailma südametunnistus? / Jeremy Rifkin ; interv. Arko Olesk

    Index Scriptorium Estoniae

    Rifkin, Jeremy

    2005-01-01

    Raamatu "European Dream" ("Euroopa unelm") autor sõnul valitseb maailmas väärarusaam Ameerika majanduse suurest jõust, mis vastandub hääbuvale ja laialilagunevale Euroopa majandusele. Tema arvates on Euroopale väljakutse see, kuidas avatakse oma uksed ulatuslikule immigratsioonile, sest seda on vaja madala iibe pärast

  1. Kuningas loodab teha kirgliku lavastuse : "Jevgeni Oneginist" saab Eesti ja Soome ooperikoolituse alustala

    Index Scriptorium Estoniae

    2002-01-01

    Sibeliuse akadeemia ja Eesti muusikaakadeemia lauluosakonna juhatajad allkirjastasid ühiste kavatsuste protokolli, mille kohaselt tuuakse ühiste jõududega välja Pjotr Tshaikovski ooper "Jevgeni Onegin"

  2. Toetuse saab äpardujalt tagasi nõuda / Kairi Oja ; kommenteerinud Lea Orro

    Index Scriptorium Estoniae

    Oja, Kairi

    2011-01-01

    PRIA peadirektor Jaan Kallas, SA Archimedes struktuuriüksuste juhataja Alice Liblik, Keskkonnainvesteeringute Keskuse kommunikatsioonijuht Kristiina Pennar, SA Innove juhatuse liige Lea Orro ning Kredexi juhataja Andrus Treier eurotoetuste tagasinõudmise põhjustest

  3. Eesti aidsiennetus saab 52 miljonit välisraha / Rando Tooming

    Index Scriptorium Estoniae

    Tooming, Rando

    2003-01-01

    Rahvusvaheline finantsorganisatsioon Global Fund (Global Fund to Fight AIDS, Tuberculosis and Malaria) annab Eestile 2 aasta jooksul aidsiennetustööks 52 miljonit krooni. Kommenteerib Nelli Kalikova

  4. Mahtras saab näha ja kuulda "Mahtra sõda" / Tõnu Tamm

    Index Scriptorium Estoniae

    Tamm, Tõnu

    2008-01-01

    30. mail Raplamaal Juurus ajaloolise Atla-Eeru kõrtsi ees toimuvast "Mahtra sõja" ettelugemisest. Mahtra sõja 150. aastapäevale pühendatud lugemisetendust lavastab Ago-Endrik Kerge. Loevad näitlejad koos eri vanuses ja eri paigust vabatahtlikega

  5. Uus punapass saab mikrokiibiga järglase / Aleksei Günter

    Index Scriptorium Estoniae

    Günter, Aleksei, 1979-

    2005-01-01

    Anti välja esimene uue kujundusega Eesti kodaniku pass, järgmisel aastal plaanib kodakondsus- ja migratsiooniamet võtta kasutusele biomeetrilise passi, mis on varustatud mikrokiibiga. Lisa: Uus pass

  6. Eesti politsei saab uued sõrmejälgede võtmise aparaadid / Olger Nõmm

    Index Scriptorium Estoniae

    Nõmm, Olger

    2005-01-01

    PHARE programmi kaasabil teostuvast AFIS-i (Automated Fingerprint Identification System) projektist, mille raames Eesti Politsei ja Piirivalveamet saavad kaasaegsed sõrmejälgede võtmise seadmed. Hangitavate seadmete tüübid. Vt. samas: Projektist on kasu kolmele ametkonnale

  7. Kas sotsiaalmeedias turundamiseks tehtud investeeringu tootlust saab mõõta? Donna L. Hoffman, Marek Fodor

    Index Scriptorium Estoniae

    Hoffmann, Donna L.

    2010-01-01

    Sotsiaalmeedia vahendusel toimuva turunduse efektiivsuse mõõtmise võimalustest. Lisatud tabel : Sotsiaalmeediarakenduste olulisemad mõõdikud, süstematiseerituna võtmetähtsusega sotsiaalmeedia eesmärkide järgi

  8. Kas terrorismi saab neutraalselt defineerida? = Is it possible to define terrorism neutrally? / Marek Järvik

    Index Scriptorium Estoniae

    Järvik, Marek

    2006-01-01

    Terrorismi definitsioon, vägivald, poliitilised eesmärgid, terrorism ja kuritegevus, avalikkus, revolutsioon ja vabadusvõitlus. Ettekanne Kaasaegse Kunsti Eesti Keskuse 4. ettekannete päeval "Kunstnike moraalsed valikud kultuurikonfliktides" Tallinna Kunstihoones 27.04.2006. Bibliograafia lk. 99

  9. Positiivsust saab õppida / Mare Pork ; intervjueerinud Signe Rummo ; kommenteerinud Toivo Aavik

    Index Scriptorium Estoniae

    Pork, Mare, 1950-

    2014-01-01

    Intervjuu Tallinna Ülikooli psühholoogiaprofessor Mare Porkiga positiivsest psühholoogiast ja raamatust Boniwell, Ilona. Positiivne psühholoogia : tõhusa toimimise põhitõed. Tallinn : Äripäev, 2014.

  10. Eesti saab tõenäoliselt USA-lt pooletoobise viisavabaduse / Raimo Poom

    Index Scriptorium Estoniae

    Poom, Raimo

    2008-01-01

    Algasid läbirääkimised USA-ga viisavabaduse saavutamiseks. USA eksperdid tulevad hindama Eesti riigipiiri pidavust, koostatakse vastastikuse arusaamise memorandum. Tõenäoliselt hakkab Eesti puhul kehtima teistsugune süsteem kui on praegu 27 riigil, kellel on USA-ga viisavabadus ja kellest 15 on EL-i nn vanad riigid. USA sisejulgeoleku ministeeriumi asekantsleri Richard Barthi seisukohti. Vt. samas: Eesti näide võib tekitada vastuolulist reaktsiooni

  11. Saksa ajaleht : Narvast saab vahest uue Euroopa inetuim linn / Sirle Sommer-Kalda

    Index Scriptorium Estoniae

    Sommer-Kalda, Sirle, 1974-

    2003-01-01

    Ilmunud ka: Severnoje Poberezhje 12. nov. lk. 1, Postimees 13. nov. lk. 5 (lüh.). Hamburgi ajalehes Hamburger Abendblatt ilmunud artiklist Narva linna kohta. Narva linnavolikogu esimehe Mihhail Stalnuhhini, linnasekretär Ants Liimetsa, sihtasutuse Pro Narva juhataja Andres Toode arvamus artiklist

  12. Regionaalareng saab tänavu seaduse / Aarne Mäe

    Index Scriptorium Estoniae

    Mäe, Aarne, 1967-

    2006-01-01

    Regionaalminister Jaan Õunapuu kinnitusel ei ole sel aastal valdade-linnade ühinemist ette näha, ehkki on olemas seaduslik baas, mille alusel kohalikud omavalitsused võivad liituda kuni 2010. aastani

  13. Hahni pubist saab kord nädalas džässiklubi / Marge Lumisalu

    Index Scriptorium Estoniae

    Lumisalu, Marge

    2009-01-01

    Eesti Draamateatri näitleja Guido Kanguri eestvõttel kõlab Pärnus C. F. Hahni pubis (Riia mnt 129a) kolmapäeviti džässmuusika. 7. oktoobril toimunud esimesel kontserdil esinenud ansamblist Ajavares

  14. Loodusfotograaf Sven Začek saab lindudega sõbraks / interv. Kristjan Roos

    Index Scriptorium Estoniae

    Začek, Sven, 1980-

    2012-01-01

    Tartu lähedal Kõrvekülas elavast 31-aastasest loodusfotograafist Sven Začekist sai Remo Savisaare ja Priit Vesilinnu kõrval kolmas eestlane, kelle fotosid on avaldanud mainekas loodusajakiri National Geographic

  15. Tallinna esimene elektrijaam saab 24. märtsil 91-aastaseks / Robert Nerman

    Index Scriptorium Estoniae

    Nerman, Robert, 1946-2015

    2004-01-01

    Tallinna Linna Elektri Keskjaama ajaloost. Elektrijaama masinajaama, katlamaja ja kontorihoone projekteeris arhitekt G. (?) Schmidt. Hoonete ehitust juhatas insener P. Kürenius. Telliskorstna rajas insener J. Russwurmi ehituskontor

  16. Skypega saab sügisest helistada sama lihtsalt kui tavatelefoniga / Henrik Roonemaa

    Index Scriptorium Estoniae

    Roonemaa, Henrik

    2004-01-01

    Eesti programmeerijate abiga loodud tasuta helistamist võimaldavast internetitelefonist Skype, mille tarbeks toob Siemens müügile spetsiaalse juhtmeta lauatelefoni koos arvuti külge käiva adapteriga

  17. Peetri maja kant Kadriorus saab peagi uue näo / Ulvar Käärt

    Index Scriptorium Estoniae

    Käärt, Ulvar, 1982-

    2009-01-01

    Kadrioru pargis asuva Peeter I maja ja presidendi kantselei vahelise pargiala uuendustöödest. Vt. samas: Presidendi lossi esine suletakse. Peetri aia rekonstrueerimistööde käigus on plaanis pargi territooriumile üle viia ka praegu presidendi kantselei esist paraadplatsi läbiv kõnnitee, kuna kantseleil on plaanis hoone esine ümbritseda piirdeaiaga

  18. Kas õpetajate professionaalne areng saab toimuda e-toel? / Piret Luik

    Index Scriptorium Estoniae

    Luik, Piret, 1967-

    2015-01-01

    Õpetajate professionaalne areng on tõusnud päevakorda kogu Euroopas ja viinud õpetajakoolituse reformimiseni. Tartu ülikooli haridusteaduste instituut koostöös partneritega Euroopa ülikoolidest kutsus personaalsemate e-kursuste loomiseks 2013. aastal ellu Lifelong Learningi projekti „Social Networks in Teacher Education” (SoNetTE)

  19. Kas talupidaja saab sõjaväest vabaks? / Carol Merzin

    Index Scriptorium Estoniae

    Merzin, Carol

    2006-01-01

    Vastab kaitseressursside ameti avalike suhete nõunik Carol Merzin. 16. apr. 2006 jõustunud kaitseväeteenistuse seaduse kohaselt võib kehvade majanduslike tingimuste korral kaitseväeteenistusest vabastamist taotleda

  20. Walesa : kommunism saab kohtupäeva / Lech Walesa ; interv. Erkki Bahovski

    Index Scriptorium Estoniae

    Walesa, Lech

    2006-01-01

    Poola kunagise vabadusliikumise Solidaarsus üks juhte, Poola endine president Lech Walesa vastab küsimustele, mis puudutavad tema autasustamist Maarjamaa Risti esimese klassi ordeniga, suhtumist endistesse kommunistidesse, Venemaa suhteid Poolaga ning Poola arengut pärast ühinemist Euroopa Liiduga. Lisa: CV

  1. Frank Lloyd Wright - väike maja saab suureks : meistriklass / Pille Nagel

    Index Scriptorium Estoniae

    Nagel, Pille

    2006-01-01

    Frank Lloyd Wrighti (1867-1959) eramuloomingust. Preeriamajadest, usonia majadest, krundist ja maastikust algavast arhitektuurist, katustest ja horisontaalsusest, plaanist, tasapindade ja kõrguste muutumistest, akendest, autovarjualustest, materjalidest ja värvidest, privaatsusest ja avatusest, inimlikust mõõtmest jm. 11 värv. vaadet, plaan

  2. Ameerika sõdurite Eestis viibimine saab selgemad reeglid / Mihkel Tamm

    Index Scriptorium Estoniae

    Tamm, Mihkel

    2017-01-01

    Eesti ja USA vahelisest kaitsekoostöö lepingust, millega kavatsetakse anda selgem raamistik USA vägede siinolekuks ja lihtsustada relvajõudude Eestis tegutsemist. Kokkuleppes pannakse paika kahe riigi suhted ja õigused, mis puudutavad näiteks Eesti kaitseväe alade ja ehitiste kasutamist, ameeriklaste maksusoodustusi, ehitusõigusi ning USA sõdurite väär- ja kriminaaltegude menetlemist

  3. Infot saab hallata kõik-ühes portaalitarkvaraga / Jaak Ennuste

    Index Scriptorium Estoniae

    Ennuste, Jaak

    2003-01-01

    Ilmunud ka: Delovõje Vedomosti 17. dets. lk. 23. Microsofti poolt turule toodud infoportaali tarkvara SharePoint Portal Server 2003 võimaldab kõiki infotöötlemise protsesse hallata ühes keskkonnas ja on mõeldud eelkõige informatsiooniga töötavatele ettevõtetele. Lisa: Portaali juurutamine ettevõttes

  4. Kuusalus saab rattad alla autotreileritööstus / Peep Talimaa

    Index Scriptorium Estoniae

    Talimaa, Peep

    2008-01-01

    OÜ-le Trucks & Trailers kuuluvast Kuusalu treileritehasest. Lisa: Kuusalu treileritehase ajalugu ja eellugu; Autotreileri valmimine; Üldandmeid treilerite kohta; Kuusalu treileritehase ajalugu ja eellugu

  5. "Vaibaparadiisist" saab puhkajate paradiis / Jukka-Pekka Pajunen ; interv. Margit Aedla

    Index Scriptorium Estoniae

    Pajunen, Jukka-Pekka

    2005-01-01

    Kinnisvarafirma Arco Vara ja Soome juhtiv vaba aja sisustaja Holiday Club Finland kavandavad Tallinnasse aastaks 2007 Põhjamaade suurimat spaahotelli. Holiday Club Finlandi projektidirektor spaade turust Eestis, Holiday City Tallinna spaa eripärast ja eelistest võrreldes teiste Eesti spaadega, selle sihtrühmast ning hindadest, Soomes tegutsevatest spaadest. Lisad: Holiday City Tallinn; Taust. Kommenteerib Arco Vara investeerimisdivisjoni projektijuht Jüri Kuusk

  6. Instituutide areng saab paika / Paavo Kaimre, Rando Värnik, Illar Lemetti, Ants Soon...[jt.

    Index Scriptorium Estoniae

    2007-01-01

    Koostatavaid arengukavasid tutvustavad Metsandus- ja maaehitusinstituudi direktor Paavo Kaimre, Majandus- ja sotsiaalinstituudi direktor Rando Värnik, Põllumajandus- ja keskkonnainstituudi direktor Illar Lemetti, Tehnikainstituudi direktor Ants Soon ja Veterinaarmeditsiini ja loomakasvatuse instituudi direktor Toomas Tiirats

  7. Mis saab ESTERMist? / Tiina Soon, Peeter Päll, Ivi Papstel ; interv. Aili Künstler

    Index Scriptorium Estoniae

    Soon, Tiina

    2008-01-01

    Eesti Õiguskeskuse loodud andmebaasist ESTERM. Vastavad EKI terminoloogiaosakonna juhataja Tiina Soon, EKI keelekorraldusosakonna vanemteadur Peeter Päll, Justiitsministeeriumi avalike suhete talituse juhataja Ivi Papstel

  8. Mahepõllumajandus saab parandada Läänemere seisundit / Anne Luik

    Index Scriptorium Estoniae

    Luik, Anne, 1949-

    2011-01-01

    BERAS projekti (Baltic Ecological Recycling Agriculture and Society Implementation) raames on esmatähtis anda edasi teadmisi, kuidas minna põllumajanduses üle ökoloogilisele taaskasutavale tootmisviisile

  9. P&G saab 57 miljardi dollari eest Gillette'i / Peeter Teder

    Index Scriptorium Estoniae

    Teder, Peeter

    2005-01-01

    Habemeajamistarvete tootjana tuntud ettevõtte Gilette'i võtab üle kaubanduse suurvalitseja Procter & Gamble, mis kujuneb ilmselt selle aasta suurimaiks ülevõtmistehinguks. Diagramm: Gilette'i aktsia aastaga tõusnud kolmandiku võrra. Vt. samas: P&G mõjukas tehing

  10. Pilistveres saab homme kohtuda Rasputiniga / Ülle Lätte

    Index Scriptorium Estoniae

    Lätte, Ülle, 1955-

    2008-01-01

    7. aug. Pilistvere vanas rehehoones esietenduvast Ain Saviaugu kirjutatud ja lavastatud suvetükist "Rasputin". Suvelavastuse toob välja Põltsamaa Teater Ellunäod koos professionaalsete näitlejatega. Nimiosas mängib näitlejast riigikogulane Indrek Saar

  11. Neli kulda juunioride MM-ilt. Mis saab edasi? / Märt Roosna

    Index Scriptorium Estoniae

    Roosna, Märt

    2006-01-01

    Juunioride kergejõustiku MM-il Pekingis võitsid eestlased neli kuldmedalit: Kaire Leibak kolmikhüppes, Marek Niit 200 m jooksus, Margus Hunt kuulitõukes ja kettaheites. Lisaks vestlus Kaire Leibaku treeneri Kersti Viruga, Marek Niiduga ja Margus Hundiga

  12. Nädalavahetusel saab alguse süvakultuuri festival "Ariel"

    Index Scriptorium Estoniae

    2008-01-01

    26.-27. okt. toimub Tallinnas V juudi süvakultuuri festival "Ariel", mille peaesinejaks on klarnetist David Krakauer ansambliga Klezmer Madness1 USAst. Lisaks annavad kontserdi solist Sofia Rubina ja ansambel Vox Clamantis

  13. Matsalu looduskaitseala saab väärilise tunnustuse / Kaire Korpe

    Index Scriptorium Estoniae

    Korpe, Kaire

    2003-01-01

    Euroopa Liidu Ministrite Nõukogu loodusliku pärandi ja bioloogilise mitmekesisuse osakonna juhataja Eladio Fernandez-Galiano annab 3. oktoobril üle rahvusvahelise aunimetuse "Euroopa kaitsealade diplom"

  14. Bob Scott: Tallinn 2011 saab oma preemiaraha kätte / Bob Scott ; intervjueerinud Teele Tammeorg

    Index Scriptorium Estoniae

    Scott, Bob

    2010-01-01

    Euroopa kultuuripealinnade hindamiskomisjoni esimees räägib oma kohtumisest Tallinna linnapea Edgar Savisaare ja kultuuriministri Laine Jänesega ning sellest, et Tallinnal ja Eestil tuleb lisatoetuse saamiseks saata Euroopa Komisjonile vaid kiri, milles nad kinnitavad, et kultuuripealinna programmi jaoks on raha olemas

  15. Eesti saab kaasaegse veiste kogumise keskuse / Lii Sammler ; kommenteerinud Aldo Vaan

    Index Scriptorium Estoniae

    Sammler, Lii, 1963-

    2016-01-01

    Oktoobris avab Eesti Tõuloomakasvatajate Ühistu Harjumaal Kaunissaares loomade kogumiskeskuse. See annab võimaluse loomad enne eksporti kokku koondada ja vajalikud uuringud teha. Vestlusest Eesti Tõuloomakasvatajate Ühistu juhatuse esimehe Tanel Bulitkoga

  16. Sillamäest saab Hollywoodi võtteplats / Teet Korsten

    Index Scriptorium Estoniae

    Korsten, Teet, 1967-

    2008-01-01

    Maria Avdjushkol on valminud komöödiafilmistsenaarium "GEP ehk Garjatshije estonskije parni" USA firma Twentieth Century Fox jaoks, teemaks eestlased Venemaal seiklemas, näitlejateks venelased ja mängupaigaks Sillamäe. Taska Film oleks Eestipoolne osanik

  17. Mis saab pärast G20-t? / Fredy-Edwin Esse

    Index Scriptorium Estoniae

    Esse, Fredy-Edwin

    2010-01-01

    G-20 finantsliidrite kohtumise järel jätkus dollari odavnemine ning kulla hind jätkas kallinemist. Mõned analüütikud loodavad kohtumisel vastu võetud otsustest stabiilsust valuutaturgudel, teiste hinnangul pole valuutasõda veel kaugeltki lõppenud

  18. Läti kunstnike näitust saab vaadata Järvamaa Muuseumis / Taive Kuuse

    Index Scriptorium Estoniae

    Kuuse, Taive

    1999-01-01

    Järvamaa muuseumis avatud läti kunstnike maalide ja keraamika näitusest, kus esinevad eesti päritolu Salduse muuseumi kunstnik Rita Armulik ning Salduse kunstikooli õpetajad Zigrida Buzoverova ja Gunta Kraulepe

  19. Tallinna ülikooli uueks südameks saab avar loovainete hoovimaja / Mari Kodres

    Index Scriptorium Estoniae

    Kodres, Mari

    2009-01-01

    Tallinna Ülikooli linnaku arhitektuurivõistluse võitsid Salto AB OÜ arhitektid Ralf Lõoke, Karli Luik ja Maarja Kask. Ülikoolil on soov kujundada peamiselt Balti Filmi- ja Meediakoolile koduks saavast hoonest ning hoovialast ülikooli uus süda. Uute õppekavadena pakub Tallinna Ülikool tuleva aasta sügisest magistritasemel infotehnoloogia ettevõtluse ja haridustehnoloogia õpet, doktoriõppe tasemel infoühiskonna tehnoloogia õpet

  20. Sänna mõisast saab kultuuri- ja loomekeskus / Kaile Kabun

    Index Scriptorium Estoniae

    Kabun, Kaile

    2009-01-01

    Sänna kultuurimõisa esimese hooaja juhatab sisse 27. veebruaril valguspidu. Mõisa õuel näeb prantsuse kunstniku valgusskulptuure. Kultuurimõisa rajamine on Rõuge vallavalitsuse ja Tallinna kultuuritehase Polymer ühisettevõtmine. Loomeinimeste residentsi ja töötubade sisseseadmise kavast

  1. Bioetanooli saab prügist / Mette Hedegaard Thomsen ; interv. Sten-Aleks Pihlak

    Index Scriptorium Estoniae

    Thomsen, Mette Hedegaard

    2008-01-01

    Taani Tehnikaülikooli Riso laboratooriumi teaduri Mette Hedegaard Thomseni sõnul suudab teise põlvkonna bioetanoolitehas teha kütust kõikvõimalikest jäätmetest ning on samas palju loodussõbralikum. Kommenteerib Robert Antropov

  2. Kiasmas saab ülevaate kaasaegse kunsti (ja elu) problemaatikast / Rael Artel

    Index Scriptorium Estoniae

    Artel, Rael, 1980-

    2005-01-01

    Seppo Renvalli retrospektiiv Taidehallis. Eksponeeritud 1990-ndate algul tehtud pinhole-säritusi, paar fotoseeriat, üle kümne 16mm kinofilmi ja video aastatest 1991-2005, installatsioon "The Ball Show" (1998-2001). Poliitilise kaasaegse kunsti väljapanek "Fractures of Life" Kiasma kollektsioonidest. Kuraatorid Tuula Karjalainen, Marja Sakari, Eija Aarnio, Leena-Maija Rossi, Erkki Berndson. Eesti kunstnike loomingust oli väljas Jaan Toomiku video "Untitled" (2001). Santiago Serra teosest

  3. Punapäisest iludusest saab Itaalia parempoolsete päästja / Tõnis Erilaid

    Index Scriptorium Estoniae

    Erilaid, Tõnis, 1943-

    2007-01-01

    Peaministrikohalt taandunud Silvio Berlusconi on väitnud, et Itaalia parempoolsete parteide ühendajaks võib saada Michele Vittoria Brambilla, kes äsja registreeris uue Vabaduspartei (Partito della Liberta)

  4. Varsti saab sada täis! : [Akadeemiline Põllumajanduse Selts] / Aimur Joandi

    Index Scriptorium Estoniae

    Joandi, Aimur, 1948-2014

    2010-01-01

    Akadeemiline Põllumajanduse Selts asutati 1920. a., lühikese aja jooksul kujunes APSist viljakas kasvulava tulevase põllumajanduskaadri ettevalmistamisel. Artiklis antakse ülevaade APSi asutamisest, põhikirjast, tegevusest, liikmetest, taastamisest 1989. a

  5. Grindeks saab Tallinna Farmaatsiatehase börsilt ära viia / Sirje Rank

    Index Scriptorium Estoniae

    Rank, Sirje, 1966-

    2005-01-01

    Tallinna Farmaatsiatehase ostnud Läti Grindeks on kätte saanud vajalikud 95% aktsiatest, mis võimaldavad firma börsilt ära viia. Diagramm: Grindeksi käive ja aktsia. Vt. samas: Lauri Matsulevitsh. Investor teenis Grindeksiga 40 000 krooni

  6. Uus äriidee - lemmik saab netti konto / Gert D. Hankewitz

    Index Scriptorium Estoniae

    Hankewitz, Gert D.

    2007-01-01

    Viis Eesti noort lõid portaali uniteddogsandcats.com, kuhu loomaomanikud saavad panna pilte oma koertest ja kassidest ning kirjutada lahti nende päevasündmusi. Vt. samas: Koer.ee omanik Hedvig Tahlfeldt: portaalidel on tulevikku. Kommenteerivad Jüri Kaljundi ja Andrei Korobeinik

  7. Mainefilmiga saab edasi anda ettevõtte reaalset olemust / Peeter Nieler

    Index Scriptorium Estoniae

    Nieler, Peeter

    2007-01-01

    Mainefilmi kui audiovisuaalse meediumi kaudu on kõige lihtsam edasi anda ettevõtte reaalset olemust, näidata selle tootmisüksusi või anda sõna tootearendajatele. Vt. samas: Mainefilmi on hea näidata messidel, jagada klientidele või näidata kodulehel

  8. Ettevõtte saab pankroti asemel uuesti jalule tõsta / Rein Lang

    Index Scriptorium Estoniae

    Lang, Rein, 1957-

    2008-01-01

    Seaduseelnõust, millega luuakse makseraskustesse sattunud firmade jaoks saneerimismenetlus, mis on alternatiiv senisele pankrotimenetlusele. Ilmunud ka Sakala 29. juuli 2008, lk. 2, pealkiri kujul: menetlus aitab makseraskustes ettevõtte jalule ; Pärnu Postimees 30. juuli 2008, lk. 15 ; Põhjarannik 29. juuli 2008, lk. 2 ; Võrumaa Teataja 31. juuli 2008, lk. 2 ; Koit 31. juuli 2008, lk. 6 ; Kuulutaja 1. august 2008, lk. 4 ; Nädaline 5. aug. 2008, lk. 4 ; Oma Saar 5. aug. 2008, lk. 5

  9. Mis saab Tallinna Polütehnikumist? / Sirje Tohver ; kommenteerib Mati Kask

    Index Scriptorium Estoniae

    Tohver, Sirje, 1948-

    2000-01-01

    Tallinna Polütehnikumi liitmisest Tallinna Kõrgema Tehnikakõrgkooliga. Arvamust avaldavad TPT õppealadirektor Jüri Mickfeldt ja AS Eesti Telefon IP Teenused turundusjuht Avo-Rein Tereping (TPT vilistlane, kooli nõukogu liige)

  10. Koolipsühholoog saab hakkama / Kärt Käesel

    Index Scriptorium Estoniae

    Käesel, Kärt

    2007-01-01

    Pelgulinna Gümnaasiumi psühholoog räägib laste probleemidest, mida ei osata märgata. Need on : terviseprobleemid, psühhiaatrilised hädad, hüperaktiivsete laste probleemid, anoreksia, koduvägivald, koolivägivald

  11. Poola saab tülis Venemaaga kogu EL-i oma selja taha / Krister Paris

    Index Scriptorium Estoniae

    Paris, Krister, 1977-

    2006-01-01

    EL-i eesistujamaa Soome lubas Poolale lisada Venemaa kehtestatud impordikeelu Poola lihatoodetele EL-i ja Venemaa läbirääkimiste ametlikku päevakorda. Impordikeelu kiiret lõpetamist toetavad Prantsusmaa ja Leedu. Lisa: Poola püüdlused "vastuvõetamatud"

  12. Ameerika pidu saab läbi / Hans-Werner Sinn

    Index Scriptorium Estoniae

    Sinn, Hans-Werner, 1948-

    2008-01-01

    Ilmunud ka: Delovõje Vedomosti 26. märts lk. 33. Jooksevkonto defitsiit, ülemäärane tarbimine ja katteta laenud USA-s on toonud lõpu ebatavaliselt pikale majanduskasvu perioodile maailmamajanduses

  13. Kas Euroopa saab Euroopaks? / Timothy Garton Ash ; tõlk. Aet Varik

    Index Scriptorium Estoniae

    Garton Ash, Timothy, 1955-

    2002-01-01

    3. aprillil 1996 peetud Sanford S. Elbergi nim. loeng California Ülikooli (Berkeley) Rahvusvaheliste Uuringute Instituudis. Euroopa määratlus enne 1945. aastat, 1945-1989, külma sõja järgsel perioodil ja tänapäeval

  14. Pathogenetical Characterization of MHV-76: a Spontaneous 9.5-Kilobase-Deletion Mutant of Murine Lymphotropic Gammaherpesvirus 68

    Directory of Open Access Journals (Sweden)

    A. Chalupková

    2008-01-01

    Full Text Available Murid gammaherpesvirus 4 (MuHV-4 provides a small animal model for the study of animal gammaherpesviruses. MHV-76 is a spontaneous deletion mutant as compared to the prototype strain of MuHV-4 (MHV-68. The MHV-76 genome lacks at least 12 ORFs at the 5'-end including the M1, M2, M3 and M4 genes and the eight viral t-RNA-like genes. During 27 months of experimental infection of BALB/c mice we followed their pathogenesis, immunology and oncogenic properties. After intranasal infection with MHV-76, the infectious virus was detected in the blood, thymus, lungs, heart, liver, spleen, bone marrow, peritoneal macrophages, lymph nodes, kidneys, mammary glands, brain and small intestine. The acute phase of infection was attenuated, but the chronic phase of infection was accompanied with long persistence of virus not only in the lymphatic, but in the neural and glandular tissue, as well. In comparison with the prototype strain, splenomegaly and lymphocytosis was very low. Surprisingly, during 27 months the BALB/c mice infected with MHV-76 did not develop lymphoproliferative disorders like infectious mononucleosis, leukaemia or lymphomas. We hypothesize that the M4 gene, present in all oncogenic MHV isolates, might be related (directly or indirectly to their transforming properties.

  15. Conversion to full sternotomy during minimal-access cardiac surgery: reasons and results during a 9.5-year experience.

    Science.gov (United States)

    Tabata, Minoru; Umakanthan, Ramanan; Khalpey, Zain; Aranki, Sary F; Couper, Gregory S; Cohn, Lawrence H; Shekar, Prem S

    2007-07-01

    A hemisternotomy approach to minimal-access cardiac surgery is associated with a faster postoperative recovery because of reduced postoperative pain and improved respiratory function. Conversion to a full sternotomy is occasionally required for reasons that remain inadequately reported. Between January 1996 and June 2005, 907 cardiac surgical patients were planned for an upper hemisternotomy and 528 for a lower hemisternotomy. We retrospectively reviewed 45 patients who required conversion to a full sternotomy. Twenty-four (2.6%) of 907 patients required a conversion from upper hemisternotomy because of bleeding (n = 8), ventricular dysfunction (n = 5), refractory ventricular arrhythmia (n = 3), poor exposure (n = 2), and other causes (n = 6). Eight (33.3%) of 24 patients died perioperatively. Of the 883 patients who went on to have an operation through the upper hemisternotomy approach, the mortality was 1.7% (15/883). Twenty-one (4.0%) of 528 patients required conversion from a lower hemisternotomy because of poor exposure (n = 16), bleeding (n = 1), refractory ventricular arrhythmia (n = 3), and a retained venous cannula (n = 1). None of these patients died postoperatively. Of the 507 patients who went on to have an operation through the lower hemisternotomy approach, the mortality was 1.2% (6/507). Conversion to a full sternotomy occurs infrequently during minimal-access cardiac surgery. Upper hemisternotomy conversions are usually urgent after crossclamp removal and are often associated with serious morbidity and mortality. Conversely, lower hemisternotomy conversions are performed electively in the prebypass period because of poor exposure and are not associated with complications.

  16. Reliability of offshore wind power production under extreme wind conditions. Deliverable D 9.5. Work Package 9: Electrical grid

    DEFF Research Database (Denmark)

    Cutululis, Nicolaos Antonio; Zeni, Lorenzo

    years, with each year simulated with five random seeds, leading to a total of 25 annual wind power time series for six large offshore wind farms, summing up to a little over 330 wind turbines. Two storm control strategies were used. The analysis involved several aspects inspired from reliability studies....... The aspects investigated are storm events occurrences and durations, storm control strategy impact on the capacity factor (lost production), the loss of production (power produced from wind drops below a certain threshold due to high wind speeds and storm controller) and finally, the wind power production......Reliability of offshore wind production under extreme wind conditions was investigated in this report. The wind power variability from existing and future large offshore wind farms in Western Denmark were simulated using the Correlated Wind model developed at Risø. The analysis was done for five...

  17. Working 9-5: Causal Relationships Between Singers' "Day Jobs" and Their Performance Work, With Implications for Vocal Health.

    Science.gov (United States)

    Bartlett, Irene; Wilson, Pat H

    2017-03-01

    It is acknowledged generally that professional contemporary commercial music (CCM) singers engage in supplementary employment ("the day job") to achieve and maintain a reliable living wage. In this paper, consideration is given to the impact of such nonperformance employment on CCM's sustainable vocal health. Collected data from a survey of 102 professional contemporary gig singers were analysed using descriptive statistical procedures from the Statistical Package for the Social Sciences. Although these data provided descriptions of the personal characteristics of individuals in the sample, the inclusion of open format questions encouraged participants to report details of their "lived" experience. Additionally, a meta-analysis of a range of associated literature was undertaken. Sixty-five participants (N = 102) reported that in addition to their heavy performance voice use, they were employed in "other" work (the "day job") where their speaking voice loads were high. In responding to open-ended questions, many proffered written comments that were unprompted. The collected data from this element of the research study are reported here. We propose that at least some causal factors of singers' reported voice problems may lie in the misuse or overuse of their everyday speaking voice (as demanded by their "day job") rather than a misuse of their singing voice. These findings have practical application to all whose concern is care for the vocal or emotional health and performance longevity of professional singers. Copyright © 2017 The Voice Foundation. Published by Elsevier Inc. All rights reserved.

  18. 3.-6. II saab neljal järjestikusel õhtul kella 18-21 imetleda valguskuplit Tallinna vanalinna kohal

    Index Scriptorium Estoniae

    2005-01-01

    Valguskupli idee pärineb hollandi arhitektilt Winy Maasilt. Installatsioon on ZiZi & YoYo, MVRDV ja Arup grupi koostööprojekt. Kupli on teostanud ZiZi & YoYo koos Rogier van de Heide, Teemu Nurmelini jt. koostööpartneritega

  19. Kommunikatsioonijuht saab aidata arsti ja patsienti / Eda Amur, Anneli Bogens, Svea Talving, Krista Valdvee ; intervjueerinud Küllike Heide

    Index Scriptorium Estoniae

    2013-01-01

    Meditsiinivaldkonna kommunikatsiooniga seotud küsimuste ja probleemide üle arutlevad nelja haigla kommunikatsioonijuhid: Eda Amur Pärnu haiglast, Anneli Bogens Ida-Viru keskhaiglast, Svea Talving Ida-Tallinna keskhaiglast ning Krista Valdvee Viljandi haiglast

  20. Toomkiriku Saueri orel saab korda! / Hugo Lepnurm, Toomas Mäeväli ; interv. Alo Põldmäe

    Index Scriptorium Estoniae

    Lepnurm, Hugo, 1914-1999

    1998-01-01

    Prof. Hugo Lepnurm ja orelimeister Toomas Mäeväli Toomkiriku Saueri oreli restaureerimise käigust saksa firmas Orgelwerkstatt Christian Scheffler. Oreli sisseõnnistamine 1. augustil 1998. Samas andmed oreli elukäigust. Oreli ehitas 1858. a. saksa meister Friedrich Ladegast. Eestis viimasel ajal töökorda saadud teistest orelitest.