Books on the topic 'Combustion chambre'

Combustion system design. Tulsa, Okla: PennWell Books, 1996.

Moon, H. J. Soot generation in a diesel combustion chamber. Manchester: UMIST, 1996.

Quentmeyer, Richard J. Rocket combustion chamber life-enhancing design concepts. [Cleveland, Ohio?]: National Aeronautics and Space Administration, Lewis Research Center, 1990.

Grigorʹev, A. V. Teorii︠a︡ kamery sgoranii︠a︡. Sankt-Peterburg: Nauka, 2010.

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

Tamaru, Takashi. Hydrogen fueled subsonic-ram-combustor model tests for an air-turbo-ram engine. Tokyo, Japan: National Aerospace Laboratory, 1990.

Hu, Tin Cheung John. An experimental and computational investigation of an annular reverse-flow combustor. [Downsview, Ont.]: University of Toronto, 1991.

Colannino, Joseph. Modeling of combustion systems: A practical approach. Boca Raton, FL: CRC/Taylor & Francis, 2006.

Gafurov, R. A. Diagnostika vnutrikamernykh prot͡s︡essov v ėnergeticheskikh ustanovkakh. Moskva: "Mashinostroenie", 1991.

Jacobs, P. A. Flow establishment in a generic scramjet combustor. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.

Modeling of combustion systems: A practical approach. Boca Raton, FL: CRC Press, 2006.

Bement, David A. Measured operating characteristics of a rectangular combustor/inlet isolator. Washington: American Institute of Aeronautics and Astronautics, 1990.

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.

Libbis, N. Coal particle behaviour in a counter-current combustor. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1987.

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.

Syed, Saadat A. Error reduction program: Final report. Cleveland, Ohio: Lewis Research Center, 1985.

Vecchiarelli, Jack. A proposed combustion chamber for approximating an isothermal heat addition process. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1992.

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.

Eurotherm Seminar (17th 1990 Cascais, Portugal). Heat transfer in radiating and combusting systems: Proceedings of Eurotherm Seminar no. 17, 8-10 October 1990, Cascais, Portugal. Berlin: Springer-Verlag, 1991.

Hu, T. C. J. An experimental and computational investigation of an annular reverse-flow combustor. [Downsview, Ont.]: Institute for Aerospace Studies, University of Toronto, 1990.

Berger, F. C. Heat transfer from propellant burning in a constant-volume chamber. [Downsview, Ont.]: Department of Aerospace Science and Engineering, University of Toronto, 1990.

I͡Arin, Leonid Petrovich. Osnovy teorii gorenii͡a dvukhfaznykh sred. Leningrad: Ėnergoatomizdat, Leningradskoe otd-nie, 1987.

Gulati, Anil. Measurement of scalar flowfield at exit of combustor sector using Raman diagnostics. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.

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

Masters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Cleveland, Ohio: Lewis Research Center, 1988.

Jankowsky, Robert S. Experimental performance of a high-area-ratio rocket nozzle at high combustion chamber pressure. [Cleveland, Ohio]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Jankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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

J, Przekwas A., and United States. National Aeronautics and Space Administration., eds. Combustion chamber analysis code: Final report. Huntsville, Ala: CFD Research Corp., 1993.

Council, Coordinating Research, Coordinating Research Council. Performance Committee., and CRC Deposit Group. Combustion Chamber Deposit Program Panel., eds. Combustion chamber deposit research tool development. Alpharetta, Ga: Coordinating Research Council, 2002.

Combustion chamber deposit research tool development. Alpharetta, Ga: Coordinating Research Council, 2002.

Center, Lewis Research, ed. Fluids and combustion facility--combustion integrated rack. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

The Coenhamworthy Combustion Handbook. CRC Press, 2012.

SSME Main Combustion Chamber (MCC) 'hot oil' dewaxing. [Washington, DC: National Aeronautics and Space Administration, 1994.

Reliability analysis of a structural ceramic combustion chamber. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Colannino, Joseph. Modeling of Combustion Systems: A Practical Approach. Taylor & Francis Group, 2006.

J, Priem Richard, and United States. National Aeronautics and Space Administration., eds. Analysis of 5 KHz combustion instabilities in 40K methane/LOX combustion chambers. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Association, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. Quincy, MA: National Fire Protection Association, 2004.

Association, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. Quincy, MA: National Fire Protection Association, 2004.

Association, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. Quincy, MA: National Fire Protection Association, 2004.

Evans, R. L. Combustion chamber design for a Lean-Burn SI engine. Society of Automotive Engineers., 1992.

1926-, Rosenberg S. D., and Lewis Research Center, eds. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. Sacramento, Calif: GenCorp, Aerojet, 1991.

Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. Sacramento, Calif: GenCorp, Aerojet, 1991.

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

R, Hicks Yolanda, Hanson Ronald K, and United States. National Aeronautics and Space Administration., eds. AST combustion workshop: Working group report. [Washington, DC]: National Aeronautics and Space Administration, 1996.

S, Jankovsky Robert, Pavli Albert J, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Hot fire test results of subscale tubular combustion chambers. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

Hot fire fatigue testing results for the compliant combustion chamber. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.

United States. National Aeronautics and Space Administration., ed. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Sacramento, Calif: Aerojet TechSystems, 1990.

United States. National Aeronautics and Space Administration., ed. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Sacramento, Calif: Aerojet TechSystems, 1990.