Books on the topic 'Gas Turbine Engine Combustion'

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.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Combustion and fuels in gas turbine engines. Neuilly sur Seine, France: AGARD, 1988.

Cawley, 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.

Bennett, J. S. Gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1986.

Fuller, E. J. Integrated CFD modeling of gas turbine combustors. Washington, D. C: AIAA, 1993.

Melconian, Jerry O. Introducing the VRT gas turbine combustor. [Washington, D.C.]: NASA, 1990.

Young, Mark F. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1988.

Veres, 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.

Bose, 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.

Yuchuan, 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.

Paxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Paxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Paxson, Daniel E. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Tacina, 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.

North 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.

Reynolds, R. Transition mixing study final report. [Washington, DC: National Aeronautics and Space Administration, 1986.

Holdeman, J. D. Mixing of multiple jets with a confined subsonic crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1997.

Gas turbine combustion. [Bristol]: Taylor and Francis, 1988.

Lefebvre, Arthur Henry. Gas turbine combustion. 2nd ed. Philadelphia: Taylor & Francis, 1999.

The handbook of microturbine generators. Tulsa, Okla: Pennwell Corp., 2003.

Aircraft gas turbine engine technology. 3rd ed. New York, N.Y: Glencoe, 1996.

Research 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.

NATO 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.

R, Ballal Dilip, ed. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.

Lefebvre, Arthur H. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.

Singh, Dr Sadhu. Industrial Combustion Engine and Gas Turbines. s k kataria, 2015.

C, 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.

United 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.

Ghojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Limited, John, 2020.

Ghojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Limited, John, 2020.

Ghojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Incorporated, John, 2020.

Ghojel, Jamil. Fundamentals of Heat Engines: Reciprocating and Gas Turbine Internal Combustion Engines. Wiley & Sons, Incorporated, John, 2020.

(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.

Lewis 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.

Grafton, Thomas A. III. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. 1987.

United 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.

Center, 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.

United 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.

United 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.

S, 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.

Center, 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.

Center, 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.

Center, 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.

United States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. Fuel-rich, catalytic reaction experimental results. [Washington, D.C.]: National Aeronautics and Space Administration, 1991.

Center, NASA Glenn Research, ed. Workshop on Aerosols and Particulates from Aircraft Gas Turbine Engines. [Cleveland, Ohio]: The Center, 1999.

E, 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.

R, 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.