Books on the topic '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.
Full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.
Find full textCawley, 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.
Find full textBennett, J. S. Gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1986.
Find full textFuller, E. J. Integrated CFD modeling of gas turbine combustors. Washington, D. C: AIAA, 1993.
Find full textMelconian, Jerry O. Introducing the VRT gas turbine combustor. [Washington, D.C.]: NASA, 1990.
Find full textYoung, Mark F. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1988.
Find full textVeres, 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.
Find full textBose, 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.
Find full textYuchuan, 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.
Find full textPaxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textPaxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textPaxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textTacina, 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.
Find full textNorth 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.
Find full textReynolds, R. Transition mixing study final report. [Washington, DC: National Aeronautics and Space Administration, 1986.
Find full textHoldeman, J. D. Mixing of multiple jets with a confined subsonic crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1997.
Find full textGas turbine combustion. [Bristol]: Taylor and Francis, 1988.
Find full textLefebvre, Arthur Henry. Gas turbine combustion. 2nd ed. Philadelphia: Taylor & Francis, 1999.
Find full textThe handbook of microturbine generators. Tulsa, Okla: Pennwell Corp., 2003.
Find full textAircraft gas turbine engine technology. 3rd ed. New York, N.Y: Glencoe, 1996.
Find full textResearch 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.
Find full textNATO 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.
Find full textR, Ballal Dilip, ed. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.
Find full textLefebvre, Arthur H. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.
Find full textSingh, Dr Sadhu. Industrial Combustion Engine and Gas Turbines. s k kataria, 2015.
Find full textC, 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.
Find full textUnited 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.
Find full textGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Limited, John, 2020.
Find full textGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Limited, John, 2020.
Find full textGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Incorporated, John, 2020.
Find full textGhojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Incorporated, John, 2020.
Find full text(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.
Find full textLewis 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.
Find full textGrafton, Thomas A. III. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. 1987.
Find full textUnited 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.
Find full textCenter, 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.
Find full textUnited 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.
Find full textUnited 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.
Find full textS, 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.
Find full textCenter, 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.
Find full textCenter, 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.
Find full textCenter, 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.
Find full textUnited States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Find full textUnited States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Find full textUnited States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.
Find full textCenter, NASA Glenn Research, ed. Workshop on Aerosols and Particulates from Aircraft Gas Turbine Engines. [Cleveland, Ohio]: The Center, 1999.
Find full textE, 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.
Find full textR, 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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