Книги з теми "Gas Turbine Engine Combustion"
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Lieuwen, Timothy C., and Vigor Yang. Combustion Instabilities In Gas Turbine Engines. Reston ,VA: American Institute of Aeronautics and Astronautics, 2006. http://dx.doi.org/10.2514/4.866807.
Повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.
Знайти повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.
Знайти повний текст джерелаCawley, James D. Phenomenological study of the behavior of some silica formers in a high velocity jet fuel burner. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.
Знайти повний текст джерелаBennett, J. S. Gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1986.
Знайти повний текст джерелаFuller, E. J. Integrated CFD modeling of gas turbine combustors. Washington, D. C: AIAA, 1993.
Знайти повний текст джерелаMelconian, Jerry O. Introducing the VRT gas turbine combustor. [Washington, D.C.]: NASA, 1990.
Знайти повний текст джерелаYoung, Mark F. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1988.
Знайти повний текст джерелаVeres, Joseph P. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаBose, S. Materials for advanced turbine engines (MATE) project 3 design, fabrication and evaluation of an oxide dispersion strengthened sheet alloy combustor liner. [Washington, DC: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаYuchuan, Liu, and Ma Gang, eds. Hang kong ran qi lun ji mo ca xue: Tribology for aero-gas turbine engines. Beijing Shi: Beijing hang kong chu ban she, 2008.
Знайти повний текст джерелаPaxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаPaxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаPaxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Знайти повний текст джерелаTacina, Robert R. Flame tube NOx emissions using a lean-direct-wall-injection combustor concept. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Знайти повний текст джерелаNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Symposium. Combustion and fuels in gas turbine engines: Papers presented at the Propulsion and Energetics Panel 70th Symposium held in Chania, Crete, Greece, on 19-23 October 1987. Neuilly-sur-Seine, France: Advisory Group for Aerospace Research & Development, 1988.
Знайти повний текст джерелаReynolds, R. Transition mixing study final report. [Washington, DC: National Aeronautics and Space Administration, 1986.
Знайти повний текст джерелаHoldeman, J. D. Mixing of multiple jets with a confined subsonic crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаGas turbine combustion. [Bristol]: Taylor and Francis, 1988.
Знайти повний текст джерелаLefebvre, Arthur Henry. Gas turbine combustion. 2nd ed. Philadelphia: Taylor & Francis, 1999.
Знайти повний текст джерелаThe handbook of microturbine generators. Tulsa, Okla: Pennwell Corp., 2003.
Знайти повний текст джерелаAircraft gas turbine engine technology. 3rd ed. New York, N.Y: Glencoe, 1996.
Знайти повний текст джерелаResearch and Technology Organization. Applied Vehicle Technology Panel. Symposium. Gas turbine engine combustion, emissions and alternative fuels =: La combustion dans les turbomoteurs, les emissions et les carburants de remplacement : papers presented at the Applied Vehicle Technology Panel Symposium organised by the former AGARD Propulsion and Energetics Panel held in Lisbon, Portugal, 12-16 October 1998. Neuilly-sur-Seine: Research and Technology Organization, 1999.
Знайти повний текст джерелаNATO Advanced Study Institute on Instrumentation for Combustion and Flow in Engines (1987 Vimeiro, Lisbon, Portugal). Instrumentation for combustion and flow in engines. Dordrecht, The Netherlands: Kluwer Academic Publishers, 1989.
Знайти повний текст джерелаR, Ballal Dilip, ed. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.
Знайти повний текст джерелаLefebvre, Arthur H. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.
Знайти повний текст джерелаSingh, Dr Sadhu. Industrial Combustion Engine and Gas Turbines. s k kataria, 2015.
Знайти повний текст джерелаC, DeLaat John, and NASA Glenn Research Center, eds. Active combustion control for aircraft gas turbine engines. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2000.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. ATTAP Advanced Turbine Technology Applications Project: 1991 annual report. Indianapolis, Ind: Allison, Gas Turbine Division, General Motors Corporation, 1992.
Знайти повний текст джерелаGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Limited, John, 2020.
Знайти повний текст джерелаGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Limited, John, 2020.
Знайти повний текст джерелаGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Incorporated, John, 2020.
Знайти повний текст джерелаGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Incorporated, John, 2020.
Знайти повний текст джерела(Editor), Timothy C. Lieuwen, and Vigor Yang (Editor), eds. Combustion Instabilities in Gas Turbine Engines: Operational Experience, Fundamental Mechanisms, And Modeling (Progress in Astronautics and Aeronautics). AIAA (American Institute of Aeronautics & Ast, 2005.
Знайти повний текст джерелаLewis Research Center. Aeropropulsion Facilities & Experiments Division, ed. Engine Research Building combustion and aerochemistry facilities. [Cleveland, Ohio?]: National Aeronautics and Space Administration, Lewis Research Center, Aeropropulsion Facilities & Experiments Division, 1994.
Знайти повний текст джерелаGrafton, Thomas A. III. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. 1987.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Combustion noise from gas turbine aircraft engines measurement of far-field levels. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаCenter, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. Turbine engine hot section technology 1986: Proceedings of a conference. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Preliminary assessment of combustion modes for internal combusiton wave rotors. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Preliminary assessment of combustion modes for internal combusiton wave rotors. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Знайти повний текст джерелаS, Samuelsen G., and United States. National Aeronautics and Space Administration., eds. Atomization and dispersion of a liquid jet injected into a crossflow of air: Under grant NAG3-1124. [Washington, DC: National Aeronautics and Space Administration, 1996.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. Overview of high-fidelity modeling activities in the numerical propulsion system simulations (NPSS) project. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2002.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаCenter, NASA Glenn Research, ed. Workshop on Aerosols and Particulates from Aircraft Gas Turbine Engines. [Cleveland, Ohio]: The Center, 1999.
Знайти повний текст джерелаE, Smith Clifford, Lai Ming-Chia, and Lewis Research Center, eds. Rapid mix concepts for low emission combustors in gas turbine engines. [Washington, D.C.]: National Aeronautics and Space Administration, 1990.
Знайти повний текст джерелаR, Hicks Y., and United States. National Aeronautics and Space Administration., eds. Imaging fluorescent combustion species in gas turbine flame tubes: On complexities in real systems. [Washington, DC]: National Aeronautics and Space Administration, 1997.
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