Книги з теми "Gas turbine combustion chambers"

Shyy, W. A numerical study of flow in gas-turbine combustor. New York: AIAA, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Advanced technology for aero gas turbine components. Neuilly sur Seine, France: AGARD, 1987.

1969-, 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.

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.

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.

Holdeman, 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.

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.

Stewart, William E. Design guide: Combustion turbine inlet air cooling systems. Atlanta, Ga: American Society of Heating, Refrigerating and Air-Conditioning Engineers, 1999.

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.

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.

Sudarev, A. V. Kamery sgoranii͡a︡ gazoturbinnykh ustanovok: Intensifikat͡s︡ii͡a︡ gorenii͡a︡. Leningrad: "Nedra," Leningradskoe otd-nie, 1990.

Sudarev, A. V. Kamery sgoranii͡a︡ gazoturbinnykh ustanovok: Teploobmen. Leningrad: "Mashinostroenie," Leningradskoe otd-nie, 1985.

D, Roy G., and International Colloquium on Control of Detonation Processes (2000 : Moscow, Russia), eds. Control of detonation processes. Moscow: Elex-KM Publishers, 2000.

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.

Symposium 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.

Jacobson, Nathan S. High-temperature durability considerations for HSCT combustor. Cleveland, Ohio: Lewis Research Center, 1992.

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

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

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.

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

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

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

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

Odgers, J. Gas turbine fuels and their influence on combustion. Turnbridge Wells, Kent: Abacus Press, 1986.

Janicka, 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.

Janicka, Johannes. Flow and Combustion in Advanced Gas Turbine Combustors. Dordrecht: Springer Netherlands, 2013.

Fuel rich catalytic combustion, the first stage of a two-stage combustor. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.

L, 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.

L, 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.

Clean combustors for industrial gas turbines: February 9-13, 2004. Rhode Saint Genese, Belgium: Von Karman Institute for Fluid Dynamics, 2004.

Mixing characteristics of directly opposed rows of jets injected normal to a crossflow in a rectangular duct. [Washington, DC: National Aeronautics and Space Administration, 1994.

C, 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.

An analytical study of dilution jet mixing in a cylindrical duct. [Washington, DC]: National Aeronautics and Space Administration, 1993.

E, 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.

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.

CFD mixing analysis of jets injected from straight and slanted slots into confined crossflow in rectangular ducts. [Washington, DC]: National Aeronautics and Space Administration, 1992.

A parametric numerical study of mixing in a cylindrical duct. [Washington, DC]: National Aeronautics and Space Administration, 1992.

United 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.

Razi, 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.

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.

Experimental study of cross flow mixing in cylindrical and rectangular ducts. [Washington, DC: National Aeronautics and Space Administration, 1993.

United 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.

Multi-dimensional measurements of combustion species in flame tube and sector gas turbine combustors. [Washington, DC]: National Aeronautics and Space Administration, 1996.