Books on the topic 'Gas turbine combustion chambers'
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Shyy, W. A numerical study of flow in gas-turbine combustor. New York: AIAA, 1987.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Advanced technology for aero gas turbine components. Neuilly sur Seine, France: AGARD, 1987.
Find full text1969-, Xu Quanhong, and Liu Gao'en 1939-, eds. Ran qi lun ji ran shao shi: Cas turbine combustor. Beijing Shi: Guo fang gong ye chu ban she, 2008.
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 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 textHoldeman, J. D. A numerical study of the effects of curvature and convergence on dilution jet mixing. [Washington, D.C.]: National Aeronautics and Space Administration, 1987.
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 textStewart, William E. Design guide: Combustion turbine inlet air cooling systems. Atlanta, Ga: American Society of Heating, Refrigerating and Air-Conditioning Engineers, 1999.
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 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 textSudarev, A. V. Kamery sgoranii͡a︡ gazoturbinnykh ustanovok: Intensifikat͡s︡ii͡a︡ gorenii͡a︡. Leningrad: "Nedra," Leningradskoe otd-nie, 1990.
Find full textSudarev, A. V. Kamery sgoranii͡a︡ gazoturbinnykh ustanovok: Teploobmen. Leningrad: "Mashinostroenie," Leningradskoe otd-nie, 1985.
Find full textD, Roy G., and International Colloquium on Control of Detonation Processes (2000 : Moscow, Russia), eds. Control of detonation processes. Moscow: Elex-KM Publishers, 2000.
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 textSymposium of the AGARD Propulsion and Energetics Panel (65th 1985 Bergen, Norway). Heat transfer and cooling in gas turbines: Papers presented at the Propulsion and Energetics Panel 65th Symposium, held in Bergen, Norway, 6-10 May 1985. Neuilly sur Seine, France: North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1985.
Find full textJacobson, Nathan S. High-temperature durability considerations for HSCT combustor. Cleveland, Ohio: Lewis Research Center, 1992.
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 textLieuwen, 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 textR, Ballal Dilip, ed. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.
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 textLefebvre, Arthur H. Gas turbine combustion: Alternative fuels and emissions. 3rd ed. Boca Raton: Taylor & Francis, 2010.
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 textOdgers, J. Gas turbine fuels and their influence on combustion. Turnbridge Wells, Kent: Abacus Press, 1986.
Find full textJanicka, Johannes, Amsini Sadiki, Michael Schäfer, and Christof Heeger, eds. Flow and Combustion in Advanced Gas Turbine Combustors. Dordrecht: Springer Netherlands, 2013. http://dx.doi.org/10.1007/978-94-007-5320-4.
Full textJanicka, Johannes. Flow and Combustion in Advanced Gas Turbine Combustors. Dordrecht: Springer Netherlands, 2013.
Find full textFuel rich catalytic combustion, the first stage of a two-stage combustor. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.
Find full textL, Yang S., Kundu K. P, and United States. National Aeronautics and Space Administration., eds. Evaluation of water injection effect on NOx formation for a staged gas turbine combustor. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.
Find full textL, Yang S., Kundu K. P, and United States. National Aeronautics and Space Administration., eds. Evaluation of water injection effect on NOx formation for a staged gas turbine combustor. Washington, D.C: American Institute of Aeronautics and Astronautics, 1996.
Find full textClean combustors for industrial gas turbines: February 9-13, 2004. Rhode Saint Genese, Belgium: Von Karman Institute for Fluid Dynamics, 2004.
Find full textMixing characteristics of directly opposed rows of jets injected normal to a crossflow in a rectangular duct. [Washington, DC: National Aeronautics and Space Administration, 1994.
Find full textC, Mongia H., Mularz Edward J, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology Activity., eds. Assessment, development, and application of combustor aerothermal models J.D. Holdeman, H.C. Mongia, and E.J. Mularz. [Washington, DC]: National Aeronautics and Space Administration ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity, 1988.
Find full textAn analytical study of dilution jet mixing in a cylindrical duct. [Washington, DC]: National Aeronautics and Space Administration, 1993.
Find full textE, Smith C., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. CFD assessment of orifice aspect ratio and mass flow ratio on jet mixing in rectangular ducts. [Washington, DC: National Aeronautics and Space Administration, 1994.
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 textCFD mixing analysis of jets injected from straight and slanted slots into confined crossflow in rectangular ducts. [Washington, DC]: National Aeronautics and Space Administration, 1992.
Find full textA parametric numerical study of mixing in a cylindrical duct. [Washington, DC]: National Aeronautics and Space Administration, 1992.
Find full textUnited States. National Aeronautics and Space Administration., ed. Mixing of multiple jets with a confined subsonic crossflow: Summary of NASA-supported experiments and modeling. [Washington, DC]: National Aeronautics and Space Administration, 1991.
Find full textRazi, Nalim M., and Lewis Research Center, eds. A modified through-flow ware rotor cycle with combustor bypass ducts. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
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 textExperimental study of cross flow mixing in cylindrical and rectangular ducts. [Washington, DC: National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Find full textMulti-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1996.
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