Добірка наукової літератури з теми "Jet engine inlet"
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Статті в журналах з теми "Jet engine inlet"
Langston, Lee S. "Jet Engine Fuel Burn Reduction Through Boundary Layer Ingestion." Mechanical Engineering 136, no. 04 (April 1, 2014): 54–58. http://dx.doi.org/10.1115/1.2014-apr-5.
Повний текст джерелаReddy, P. Nithish. "Hypersonic Scram-Jet Engine Inlet Design." International Journal for Research in Applied Science and Engineering Technology 7, no. 6 (June 30, 2019): 1619–35. http://dx.doi.org/10.22214/ijraset.2019.6273.
Повний текст джерелаSmith, Jerome P., Ricardo A. Burdisso, and Chris R. Fuller. "Active control of jet engine inlet noise." Journal of the Acoustical Society of America 101, no. 5 (May 1997): 3122. http://dx.doi.org/10.1121/1.418918.
Повний текст джерелаBiglarian, M., A. Najafi, and S. M. Negharchi. "Numerical Analysis of inlet vortex in the scaled engine." IOP Conference Series: Materials Science and Engineering 1196, no. 1 (October 1, 2021): 012033. http://dx.doi.org/10.1088/1757-899x/1196/1/012033.
Повний текст джерелаTam, Christopher K. W., Sarah A. Parrish, Edmane Envia, and Eugene W. Chien. "Physical processes influencing acoustic radiation from jet engine inlets." Journal of Fluid Mechanics 725 (May 14, 2013): 152–94. http://dx.doi.org/10.1017/jfm.2013.181.
Повний текст джерелаPečinka, Jiří, Gabriel Thomas Bugajski, Petr Kmoch, and Adolf Jílek. "JET ENGINE INLET DISTORTION SCREEN AND DESCRIPTOR EVALUATION." Acta Polytechnica 57, no. 1 (February 28, 2017): 22–31. http://dx.doi.org/10.14311/ap.2017.57.0022.
Повний текст джерелаZhao, Xue Jun, Xiao Guo Guo, and Chang Zhao. "A New Support Structure in Waverider Force Measurement." Applied Mechanics and Materials 318 (May 2013): 96–99. http://dx.doi.org/10.4028/www.scientific.net/amm.318.96.
Повний текст джерелаBazazzadeh, Mehrdad, and Ali Shahriari. "Enhancing the Performance of Jet Engine Fuel Controller Using Neural Networks." Applied Mechanics and Materials 390 (August 2013): 393–97. http://dx.doi.org/10.4028/www.scientific.net/amm.390.393.
Повний текст джерелаCatana, Razvan Marius, and Grigore Cican. "Study of Air Excess in Relation with Engine Parameters for a Generalized Reaction Based on JET-A Fuel." Applied Mechanics and Materials 772 (July 2015): 395–400. http://dx.doi.org/10.4028/www.scientific.net/amm.772.395.
Повний текст джерелаFukuda, Masafumi, Hiroshi Harada, Tadaharu Yokokawa, and Tomonori Kitashima. "Virtual Jet Engine System." Materials Science Forum 638-642 (January 2010): 2239–44. http://dx.doi.org/10.4028/www.scientific.net/msf.638-642.2239.
Повний текст джерелаДисертації з теми "Jet engine inlet"
Hoopes, Kevin M. "A New Method for Generating Swirl Inlet Distortion for Jet Engine Research." Thesis, Virginia Tech, 2013. http://hdl.handle.net/10919/49545.
Повний текст джерелаA new method capable of recreating any arbitrary swirl distortion profile is needed in order to expand the capabilities of inlet distortion testing. This will allow designers to explore how an engine would react to a particular engine airframe combination as well as methods for creating swirl distortion tolerant engines. The following material will present such a method as well as experimental validation of its effectiveness.
Master of Science
Kumar, Abhinav. "Flow control optimization in a jet engine serpentine inlet duct." [College Station, Tex. : Texas A&M University, 2007. http://hdl.handle.net/1969.1/ETD-TAMU-1399.
Повний текст джерелаTichenor, Nathan Ryan. "Particle image velocimetry in an advanced, serpentine jet engine inlet duct." Thesis, [College Station, Tex. : Texas A&M University, 2007. http://hdl.handle.net/1969.1/ETD-TAMU-1401.
Повний текст джерелаKirk, Aaron Michael. "Active flow control in an advanced serpentine jet engine inlet duct." [College Station, Tex. : Texas A&M University, 2006. http://hdl.handle.net/1969.1/ETD-TAMU-1027.
Повний текст джерелаReilly, Daniel. "An Investigation into Jet Engine Inlet Flow Characteristics for Turbine-Powered Helicopters." The Ohio State University, 2015. http://rave.ohiolink.edu/etdc/view?acc_num=osu1429608968.
Повний текст джерелаYarlagadda, Santosh. "Performance Analysis of J85 Turbojet Engine Matching Thrust with Reduced Inlet Pressure to the Compressor." University of Toledo / OhioLINK, 2010. http://rave.ohiolink.edu/etdc/view?acc_num=toledo1271367584.
Повний текст джерелаGiuliani, James Edward. "Jet Engine Fan Response to Inlet Distortions Generated by Ingesting Boundary Layer Flow." The Ohio State University, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=osu1468564279.
Повний текст джерелаSivapragasam, M. "Numerical and experimental investigations on multiple air jets in counterflow for generating aircraft gas turbine engine inlet flow distortion patterns." Thesis, Coventry University, 2014. http://curve.coventry.ac.uk/open/items/0ad1d0c2-6693-4c6e-9224-5a2237862074/1.
Повний текст джерелаClark, Adam. "Predicting the Crosswind Performance of High Bypass Ratio Turbofan Engine Inlets." The Ohio State University, 2016. http://rave.ohiolink.edu/etdc/view?acc_num=osu1476265135449178.
Повний текст джерелаLambie, David. "Inlet distortion and turbofan engines." Thesis, University of Cambridge, 1989. http://ethos.bl.uk/OrderDetails.do?uin=uk.bl.ethos.305300.
Повний текст джерелаКниги з теми "Jet engine inlet"
Steenken, William G. An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: NASA Dryden Flight Research Center, 1997.
Знайти повний текст джерелаTrefny, Charles J. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. Cleveland, Ohio: Lewis Research Center, 1986.
Знайти повний текст джерелаPowell, A. G. Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot. [Washington, DC]: National Aeronautics and Space Administration, 1985.
Знайти повний текст джерелаPowell, A. G. Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot. [Washington, DC]: National Aeronautics and Space Administration, 1985.
Знайти повний текст джерелаPowell, A. G. Low-speed aerodynamic test of an axisymmetric supersonic inlet with variable cowl slot. [Washington, DC]: National Aeronautics and Space Administration, 1985.
Знайти повний текст джерелаB, True, Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Effects of initial conditions on a single jet in crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаE, Neumann Harvey, Shaw Robert J. 1946-, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Performance and surge limits of a TF30-P-3 turbofan engine/axisymmetric mixed-compression inlet propulsion system at Mach 2.5. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Знайти повний текст джерелаP, Myers Lawrence, Mackall Karen G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Effects of inlet distortion on a static pressure probe mounted on the engine hub in an F-15 airplane. Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.
Знайти повний текст джерелаNASA Dryden Flight Research Center., ed. An inlet distortion assessment during aircraft departures at high angle of attack for an F/A-18A aircraft. Edwards, Calif: NASA Dryden Flight Research Center, 1997.
Знайти повний текст джерелаW, Wasserbauer Joseph, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch., eds. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаЧастини книг з теми "Jet engine inlet"
Decher, Reiner. "More Components: Inlets, Mixers, and Nozzles." In The Vortex and The Jet, 137–54. Singapore: Springer Singapore, 2022. http://dx.doi.org/10.1007/978-981-16-8028-1_13.
Повний текст джерелаTheune, Marius, Dirk Schönweitz, and Rainer Schnell. "Sensitivity of a Low Pressure Ratio Jet Engine Fan to Inlet Distortion." In Notes on Numerical Fluid Mechanics and Multidisciplinary Design, 63–73. Cham: Springer International Publishing, 2016. http://dx.doi.org/10.1007/978-3-319-27279-5_6.
Повний текст джерелаТези доповідей конференцій з теми "Jet engine inlet"
Al-Khalil, Kamel, Theo Keith, Jr., and Kenneth De Witt. "Icing calculations on a typical commercial jet engine inlet nacelle." In 32nd Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1994. http://dx.doi.org/10.2514/6.1994-610.
Повний текст джерелаBalepin, Vladimir, and Glenn Liston. "The Steam Jet - Mach 6+ turbine engine with inlet air conditioning." In 37th Joint Propulsion Conference and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2001. http://dx.doi.org/10.2514/6.2001-3238.
Повний текст джерелаBEALE, D., and M. S. COLLIER. "Validation of a free-jet technique for evaluating inlet-engine compatibility." In 25th Joint Propulsion Conference. Reston, Virigina: American Institute of Aeronautics and Astronautics, 1989. http://dx.doi.org/10.2514/6.1989-2325.
Повний текст джерелаAl-Khalil, Kamel, Richard Hitzigrath, Oliver Philippi, and Colin Bidwell. "Icing analysis and test of a business jet engine inlet duct." In 38th Aerospace Sciences Meeting and Exhibit. Reston, Virigina: American Institute of Aeronautics and Astronautics, 2000. http://dx.doi.org/10.2514/6.2000-1040.
Повний текст джерелаFujii, Akira, Shinichi Mizuno, Hironori Horiguchi, and Yoshinobu Tsujimoto. "Suppression of Cavitation Instabilities by Jet Injection at Inducer Inlet." In ASME 2005 Fluids Engineering Division Summer Meeting. ASMEDC, 2005. http://dx.doi.org/10.1115/fedsm2005-77380.
Повний текст джерелаNaseri, A., M. Boroomand, A. M. Tousi, and A. R. Alihosseini. "The Effect of Inlet Flow Distortion on Performance of a Micro-Jet Engine: Part 2 — Engine Tests." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-86803.
Повний текст джерелаKrasheninnikov, S. Yu, and D. E. Pudovikov. "Analysis of the reverse jet influence on particle ingestion at the engine inlet." In Progress in Flight Physics – Volume 7, edited by D. Knight, I. Lipatov, and P. Reijasse. Les Ulis, France: EDP Sciences, 2015. http://dx.doi.org/10.1051/eucass/201507283.
Повний текст джерелаTasic, Miodrag, Branko Kolundzija, and Tomislav Milosevic. "Domain decomposition method for scattering from an aircraft with jet engine inlet cavity." In 2018 International Applied Computational Electromagnetics Society Symposium (ACES). IEEE, 2018. http://dx.doi.org/10.23919/ropaces.2018.8364325.
Повний текст джерелаNaseri, A., M. Boroomand, and A. M. Tousi. "The Effect of Inlet Flow Distortion on Performance of a Micro-Jet Engine: Part 1 — Development of an Inlet Simulator." In ASME 2012 International Mechanical Engineering Congress and Exposition. American Society of Mechanical Engineers, 2012. http://dx.doi.org/10.1115/imece2012-86865.
Повний текст джерелаMorton, Wayne K., Glen R. Lazalier, C. Dennis Rose, and R. F. (Pete) Lauer. "On-Line Distortion Analysis System for Inlet-Engine Testing." In ASME 1991 International Gas Turbine and Aeroengine Congress and Exposition. American Society of Mechanical Engineers, 1991. http://dx.doi.org/10.1115/91-gt-166.
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