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Relevant bibliographies by topics / Jet facility

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Dissertations / Theses
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Academic literature on the topic 'Jet facility'

Author: Grafiati

Published: 4 June 2021

Last updated: 6 February 2022

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Journal articles on the topic "Jet facility"

1

Kaye, Alan S., M. Cox, J. W. Farthing, M. Hitchin, and P. Lomas. "Operation of JET as a user facility." Fusion Engineering and Design 66-68 (September 2003): 175–79. http://dx.doi.org/10.1016/s0920-3796(03)00213-8.

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Perevezentsev, A. N., and A. C. Bell. "Development of Water Detritiation Facility for JET." Fusion Science and Technology 53, no. 3 (2008): 816–29. http://dx.doi.org/10.13182/fst08-a1737.

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3

Subramanian, Vishwanath, and Vinod B. Makhijani. "A test facility for a plane jet." International Communications in Heat and Mass Transfer 12, no. 5 (1985): 551–58. http://dx.doi.org/10.1016/0735-1933(85)90078-8.

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Shapira, D., J. L. C. Ford, R. Novotny, B. Shivakumar, R. L. Parks, and S. T. Thornton. "The HHIRF supersonic gas jet target facility." Nuclear Instruments and Methods in Physics Research Section A: Accelerators, Spectrometers, Detectors and Associated Equipment 228, no. 2-3 (1985): 259–66. http://dx.doi.org/10.1016/0168-9002(85)90267-0.

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Perevezentsev, A. N., A. C. Bell, P. D. Brennan, and J. L. Hemmerich. "Development of a water detritiation facility for JET." Fusion Engineering and Design 61-62 (November 2002): 585–89. http://dx.doi.org/10.1016/s0920-3796(02)00253-3.

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Loupias, B., E. Falize, M. Koenig, et al. "Plasma Jet Experiments Using LULI 2000 Laser Facility." Astrophysics and Space Science 307, no. 1-3 (2006): 103–7. http://dx.doi.org/10.1007/s10509-006-9249-y.

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Ahuja, K. K. "Designing Clean Jet-Noise Facilities and Making Accurate Jet-Noise Measurements." International Journal of Aeroacoustics 2, no. 3 (2003): 371–412. http://dx.doi.org/10.1260/147547203322986188.

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The main objective of this paper is to provide guidelines for designing and calibrating a high quality, static, jet-noise research facility and making high-quality jet noise measurements. Particular emphasis is placed on methodology for determining if internal noise is dominant in the jet noise spectrum. A section of this document is devoted to clarifying the terminology associated with microphone frequency response corrections and providing a step-wise description of other corrections that must be applied to the measured raw spectra before the jet noise data can be considered accurate and rea

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Rosen, P. A., J. M. Foster, R. J. R. Williams, et al. "Laboratory-astrophysics jet experiments at the omega laser facility." Journal de Physique IV (Proceedings) 133 (June 2006): 1019–23. http://dx.doi.org/10.1051/jp4:2006133206.

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Duesing, G. "The vacuum systems of the nuclear fusion facility JET." Vacuum 37, no. 3-4 (1987): 309–15. http://dx.doi.org/10.1016/0042-207x(87)90015-7.

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Chakrabarti, A., A. Bandyopadhyay, Arup Bandyopadhyay, et al. "The helium-jet coupled ISOL facility at VECC, Calcutta." Nuclear Instruments and Methods in Physics Research Section B: Beam Interactions with Materials and Atoms 70, no. 1-4 (1992): 254–58. http://dx.doi.org/10.1016/0168-583x(92)95940-s.

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Dissertations / Theses on the topic "Jet facility"

1

Robertson, Peter R. Van Treuren Kenneth W. "The design and validation of an impinging jet test facility." Waco, Tex. : Baylor University, 2005. http://hdl.handle.net/2104/3008.

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Maraoui, André. "Aerothermodynamic analysis of a Coanda/Refraction jet engine test facility." Thesis, Monterey, California. Naval Postgraduate School, 1988. http://hdl.handle.net/10945/22863.

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Approved for public release; distribution is unlimited<br>A computer model of the Coanda Refraction Jet Engine Test Cell facility was developed using the PHOENICS computer code. The PIIOENICS code was utilized to determine the steady state aerothermal characteristics of the test cell during the testing of an E404 gas turbine engine with afterburner in operation. Computer generated aerothermodynamic field variables of pressure, velocity and temperature parameters were compared to operational field test data. Observations regarding compared results as well as system behavior are presented.

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Ratner, Todd G. "Parametric study of the aerothermodynamics of a jet engine test facility." Thesis, Monterey, California. Naval Postgraduate School, 1989. http://hdl.handle.net/10945/27199.

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A three-dimensional numerical analysis of the Jet Engine Hush House located at Naval Air Station Jacksonville, Florida was developed using the PHOENICS computer code. The PHOENICS code was used to determine the steady state aerothermal characteristics in the Hush House produced by a Navy F-4 (Phantom II) J-79-GE-8 gas turbine engine with afterburner. The PHOENICS generated pressure, velocity, and temperature fields of the test cell facility based on the k-epsilon turbulence model are compared with results generated by a model incorporating a temperature dependent kinematic turbulent viscosity.

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Hahn, Casey Bernard. "Design and Validation of the New Jet Facility and Anechoic Chamber." The Ohio State University, 2011. http://rave.ohiolink.edu/etdc/view?acc_num=osu1311877224.

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Burger, Victor. "The design of a combustion test facility for synthetic jet fuel research." Master's thesis, University of Cape Town, 2009. http://hdl.handle.net/11427/9495.

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Includes bibliographical references (p. 78-80).<br>With the relatively recent emergence of non-petroleum-derived aviation gas turbine fuels, it was appropriate to review the complete list of jet-fuel specifications to assess whether they were sufficiently robust to ensure fit-forpurpose within the new paradigm. Although this has been an industry-wide endeavour, there were some particular research areas that were identified for special in-house attention by Sasol, as the worldâ€™s first commercial producer of approved and certified semi-synthetic and fully synthetic jet fuel. The project descri

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Mills, John Richard. "A mach 1.95 free-jet facility for experimental investigation of injectant flow patterns." Thesis, Virginia Tech, 1991. http://hdl.handle.net/10919/41997.

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Mahon, Patrick Gerard. "Development of a testing facility for verification of radial turbine design procedures and off-design performance predictions." Thesis, Queen's University Belfast, 1991. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.334483.

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Yeow, Tze Wei. "Integration of an expert system and experimental facility for advanced anti-G protection of jet fighter pilots." Thesis, National Library of Canada = Bibliothèque nationale du Canada, 2000. http://www.collectionscanada.ca/obj/s4/f2/dsk1/tape3/PQDD_0031/MQ63248.pdf.

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Eriksson, Benjamin. "Simulations of a back scatter time of flight neutron spectrometer for the purpose of concept testing at the NESSA facility." Thesis, Uppsala universitet, Tillämpad kärnfysik, 2018. http://urn.kb.se/resolve?urn=urn:nbn:se:uu:diva-359981.

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A back scatter time of flight neutron spectrometer consisting of two scintillation detectors is simulated in Geant4 to examine whether it is possible to perform a proof of concept test at the NESSA facility at Uppsala University. An efficiency of ε = 2.45 · 10^-6 is shown to be large enough for a neutron generator intensity of 1.9 · 10^10 neutrons per second to achieve a minimal required signal count rate of 10000 counts per hour. A corresponding full width at half maximum energy resolution of 8.3% is found. The background in one of the detectors is simulated in MCNP and found to be a factor 6

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Keltner, Erik. "A two-phase heat transfer test facility for ammonia : construction and testing." Thesis, Manhattan, Kan. : Kansas State University, 2005. http://hdl.handle.net/2097/113.

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Books on the topic "Jet facility"

1

Maraoui, Andre. Aerothermodynamic analysis of a Coanda/Refraction jet engine test facility. Naval Postgraduate School, 1988.

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Ratner, Todd G. Parametric study of the aerothermodynamics of a jet engine test facility. Naval Postgraduate School, 1989.

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3

Carty, Atherton A. Development and validation of a supersonic helium-air coannular jet facility. National Aeronautics and Space Administration, Langley Research Center, 1999.

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Tucker, Tom. Touchdown: The development of propulsion controlled aircraft at NASA Dryden. NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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Tom, Tucker. Touchdown: The development of propulsion controlled aircraft at NASA Dryden. NASA History Office, Office of Policy and Plans, NASA Headquarters, 1999.

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Robinson, Raymond C. Hot corrosion test facility at the NASA Lewis Special Projects Laboratory. National Aeronautics and Space Administration, 1994.

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Yeow, Tze wei. Integration of an expert system and experimental facility for advanced anti-G protection of jet fighter pilots. National Library of Canada, 2000.

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8

Day, Richard E. Coupling dynamics in aircraft: A historical perspective. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1997.

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US GOVERNMENT. An Act to Redesignate the Facility of the United States Postal Service Located at 514 Express Center Road in Chicago, Illinois, as the "J.T. Weeker Service Center.". U.S. G.P.O., 2000.

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Office, General Accounting. Depot maintenance: Future year estimates of public and private workloads are likely to change : report to the Chairman, Subcommittee on Military Readiness, Committee on Armed Services, House of Representatives. The Office, 2000.

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Book chapters on the topic "Jet facility"

1

Sunny, Kalakanda Alfred, Nallapaneni Manoj Kumar, Aldin Justin, and M. Harithra. "Development of Single and Multi-jet Conical Nozzle Based Open Jet Facility for Cold Jet Simulation." In Advances in Intelligent Systems and Computing. Springer Singapore, 2017. http://dx.doi.org/10.1007/978-981-10-5520-1_29.

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Parameshwari, S., Pradeep Kumar, S. Thanigaiarasu, and E. Rathakrishnan. "Experimental Investigation of Twin Elliptic Orifice Using High Speed Jet Facility." In Lecture Notes in Mechanical Engineering. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-3631-1_4.

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Kirchheck, Daniel, Dominik Saile, and Ali Gülhan. "Rocket Wake Flow Interaction Testing in the Hot Plume Testing Facility (HPTF) Cologne." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design. Springer International Publishing, 2020. http://dx.doi.org/10.1007/978-3-030-53847-7_9.

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Abstract Rocket wake flows were under investigation within the Collaborative Research Centre SFB/TRR40 since the year 2009. The current paper summarizes the work conducted during its third and final funding period from 2017 to 2020. During that phase, focus was laid on establishing a new test environment at the German Aerospace Center (DLR) Cologne in order to improve the similarity of experimental rocket wake flow–jet interaction testing by utilizing hydrogen–oxygen combustion implemented into the wind tunnel model. The new facility was characterized during tests with the rocket combustor model HOC1 in static environment. The tests were conducted under relevant operating conditions to demonstrate the design’s suitability. During the first wind tunnel tests, interaction of subsonic ambient flow at Mach 0.8 with a hot exhaust jet of approx. 920 K was compared to previously investigated cold plume interaction tests using pressurized air at ambient temperature. The comparison revealed significant differences in the dynamic response of the wake flow field on the different types of exhaust plume simulation.

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Wu, Feng, Limin Gao, Xinyun Wu, Xudong Feng, Lintao Leng, and Yaoyu Li. "Aerodynamic Modeling and Transient Performance Improvement of a Free Jet Altitude Test Facility." In Communications in Computer and Information Science. Springer Singapore, 2020. http://dx.doi.org/10.1007/978-981-15-8101-4_55.

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Zhao, Ling, Xin Zhang, Bin Qi, and Yanghui Zou. "An Experimental and Computational Study of Freestream Condition in an Oxygen/Oil Gas-Jet Facility." In Lecture Notes in Electrical Engineering. Springer Singapore, 2019. http://dx.doi.org/10.1007/978-981-13-3305-7_148.

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CAIRA, Déborah. "Une pédagogie innovante." In Formation linguistique des apprenants allophones et pédagogies innovantes. Editions des archives contemporaines, 2021. http://dx.doi.org/10.17184/eac.4156.

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L’augmentation des flux migratoires, en France, depuis les années 60, a amené notre pays à promouvoir une politique linguistique d’intégration à destination des migrants allophones. Pour répondre à cette demande, l’Éducation nationale a mis en place, en 2008, le dispositif « Ouvrir l’École aux Parents pour la Réussite des Enfants » (MEN, 2017). Il s’adresse aux familles les plus éloignées du système éducatif français. Ma contribution vise à rendre compte de cette initiative tout en soulevant quelques réflexions didactiques et pédagogiques afin de faciliter et encourager sa mise en place. L’enjeu de cet article est ainsi de répondre à la problématique suivante : comment favoriser l’apprentissage/acquisition du français par des adultes migrants allophones via un dispositif coéducatif ? En effet, outre l’intégration linguistique, c’est la réussite des élèves qui est en jeu et ce, par l’implication des parents dans la scolarité de leur enfant (Vatz-Laaroussi - al., 2005 ; Vatz-Laaroussi - Kanouté, 2013). La conduite de cette opération durant deux années consécutives m’a poussée à mettre en perspective les préconisations officielles au regard de la didactique des langues (Vigner, 2001 ; Adami, 2009). Cet article ambitionne ainsi de contribuer à une meilleure promotion de cette pédagogie dite « innovante » à destination des adultes migrants en faveur d’un partenariat famille-école au bénéfice de la réussite scolaire des élèves allophones (Manigand, 1993 ; Akinci, 2016).

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Conference papers on the topic "Jet facility"

1

Gilchrist, R., and J. Naughton. "The design of a swirling jet facility." In 40th AIAA Aerospace Sciences Meeting & Exhibit. American Institute of Aeronautics and Astronautics, 2002. http://dx.doi.org/10.2514/6.2002-442.

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Albertson, Cindy, and Saied Emami. "Alleviation of facility/engine interactions in an open-jet scramjet test facility." In 37th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3677.

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Kim, Chun, Minsoo Yoon, Soo Yang, and Dae Lee. "An altitude test facility for small jet engines." In 37th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3680.

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Balboni, John, Tahir Gokcen, Frank Hui, Jaswinder Taunk, Eric Noyes, and Daniel Schickele. "Calibration of the Truncated Panel Test Arc-Jet Facility." In 41st AIAA Thermophysics Conference. American Institute of Aeronautics and Astronautics, 2009. http://dx.doi.org/10.2514/6.2009-4090.

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LONG, MARY. "Experimental investigation of an ejector-powered free-jet facility." In 28th Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1992. http://dx.doi.org/10.2514/6.1992-3569.

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Kinzie, Kevin, Brenda Henderson, and Henry Haskin. "Aeroacoustic Characteristics of Model Jet Test Facility Flow Conditioners." In 11th AIAA/CEAS Aeroacoustics Conference. American Institute of Aeronautics and Astronautics, 2005. http://dx.doi.org/10.2514/6.2005-3055.

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Marec, Ricardo, Manuel Rodrigue, Manuel San Segundo, and Belen Mingue. "Thrust correction on jet engines in sea level test facility." In 34th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-3109.

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Elavarasan, R., L. Lourenco, L. Venkatakrishnan, and A. Krothapalli. "Application of PIV to large scale STOVL supersonic jet facility." In 37th Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1999. http://dx.doi.org/10.2514/6.1999-271.

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DUESTERHAUS, D., and P. MAYWALD. "Free-jet test capability for the aeropropulsion systems test facility." In 25th Joint Propulsion Conference. American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2537.

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Park, Chung, Mark Newfield, Douglas Fletcher, and Tahir Gokcen. "Spectroscopic measurements of the flows in an arc-jet facility." In 36th AIAA Aerospace Sciences Meeting and Exhibit. American Institute of Aeronautics and Astronautics, 1998. http://dx.doi.org/10.2514/6.1998-893.

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Reports on the topic "Jet facility"

1

Wasem, Mike. ARM Aerial Facility Challenger 850 Research Jet. Office of Scientific and Technical Information (OSTI), 2019. http://dx.doi.org/10.2172/1576568.

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Skone, Timothy J. Petroleum Based Kerosene Jet Fuel Energy Conversion Facility. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509178.

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Skone, Timothy J. CBTL, 0% Biomass Fischer-Tropsch Jet Fuel Production Facility. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509006.

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Skone, Timothy J. CBTL, 10% Chipped Biomass, Fischer-Tropsch Jet Fuel Production Facility. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509255.

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Skone, Timothy J. CBTL, 20% Chipped Biomass, Fischer-Tropsch Jet Fuel Production Facility. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509257.

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Skone, Timothy J. CBTL, 20% Torrefied Biomass, Fischer-Tropsch Jet Fuel Production Facility. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509258.

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Skone, Timothy J. CBTL, 10% Torrefied Biomass, Fischer-Tropsch Jet Fuel Production Facility. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509256.

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Skone, Timothy J. CBTL, 10% Biomass, Microchipped, Separate Gasifiers, Fischer-Tropsch Jet Fuel Production Facility. Office of Scientific and Technical Information (OSTI), 2012. http://dx.doi.org/10.2172/1509254.

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Smith, Douglas R. Synthetic Jet Flow Control in a Matched-Index-of-Refraction Flow Facility. Defense Technical Information Center, 2010. http://dx.doi.org/10.21236/ada563071.

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PARSONS ENGINEERING SCIENCE INC AUSTIN TX. Plan A Assessment Report for Jet Fuel Storage Tank Number 20, Randolph AFB, Texas, LPST ID NUMBER 104626, Facility ID Number 32523. Defense Technical Information Center, 1996. http://dx.doi.org/10.21236/ada382393.

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