Bücher zum Thema „Combustion chambre“
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Combustion system design. Tulsa, Okla: PennWell Books, 1996.
Den vollen Inhalt der Quelle findenMoon, H. J. Soot generation in a diesel combustion chamber. Manchester: UMIST, 1996.
Den vollen Inhalt der Quelle findenQuentmeyer, Richard J. Rocket combustion chamber life-enhancing design concepts. [Cleveland, Ohio?]: National Aeronautics and Space Administration, Lewis Research Center, 1990.
Den vollen Inhalt der Quelle findenGrigorʹev, A. V. Teorii︠a︡ kamery sgoranii︠a︡. Sankt-Peterburg: Nauka, 2010.
Den vollen Inhalt der Quelle findenShyy, W. A numerical study of flow in gas-turbine combustor. New York: AIAA, 1987.
Den vollen Inhalt der Quelle findenTamaru, Takashi. Hydrogen fueled subsonic-ram-combustor model tests for an air-turbo-ram engine. Tokyo, Japan: National Aerospace Laboratory, 1990.
Den vollen Inhalt der Quelle findenHu, Tin Cheung John. An experimental and computational investigation of an annular reverse-flow combustor. [Downsview, Ont.]: University of Toronto, 1991.
Den vollen Inhalt der Quelle findenColannino, Joseph. Modeling of combustion systems: A practical approach. Boca Raton, FL: CRC/Taylor & Francis, 2006.
Den vollen Inhalt der Quelle findenGafurov, R. A. Diagnostika vnutrikamernykh prot͡s︡essov v ėnergeticheskikh ustanovkakh. Moskva: "Mashinostroenie", 1991.
Den vollen Inhalt der Quelle findenJacobs, P. A. Flow establishment in a generic scramjet combustor. Hampton, Va: Institute for Computer Applications in Science and Engineering, 1990.
Den vollen Inhalt der Quelle findenModeling of combustion systems: A practical approach. Boca Raton, FL: CRC Press, 2006.
Den vollen Inhalt der Quelle findenBement, David A. Measured operating characteristics of a rectangular combustor/inlet isolator. Washington: American Institute of Aeronautics and Astronautics, 1990.
Den vollen Inhalt der Quelle finden1969-, Xu Quanhong, und Liu Gao'en 1939-, Hrsg. Ran qi lun ji ran shao shi: Cas turbine combustor. Beijing Shi: Guo fang gong ye chu ban she, 2008.
Den vollen Inhalt der Quelle findenLibbis, N. Coal particle behaviour in a counter-current combustor. Haifa: Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1987.
Den vollen Inhalt der Quelle findenHoldeman, 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.
Den vollen Inhalt der Quelle findenSyed, Saadat A. Error reduction program: Final report. Cleveland, Ohio: Lewis Research Center, 1985.
Den vollen Inhalt der Quelle findenVecchiarelli, Jack. A proposed combustion chamber for approximating an isothermal heat addition process. Ottawa: National Library of Canada = Bibliothèque nationale du Canada, 1992.
Den vollen Inhalt der Quelle findenBose, 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.
Den vollen Inhalt der Quelle findenEurotherm 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.
Den vollen Inhalt der Quelle findenHu, T. C. J. An experimental and computational investigation of an annular reverse-flow combustor. [Downsview, Ont.]: Institute for Aerospace Studies, University of Toronto, 1990.
Den vollen Inhalt der Quelle findenBerger, F. C. Heat transfer from propellant burning in a constant-volume chamber. [Downsview, Ont.]: Department of Aerospace Science and Engineering, University of Toronto, 1990.
Den vollen Inhalt der Quelle findenI͡Arin, Leonid Petrovich. Osnovy teorii gorenii͡a dvukhfaznykh sred. Leningrad: Ėnergoatomizdat, Leningradskoe otd-nie, 1987.
Den vollen Inhalt der Quelle findenGulati, Anil. Measurement of scalar flowfield at exit of combustor sector using Raman diagnostics. Washington, D. C: American Institute of Aeronautics and Astronautics, 1992.
Den vollen Inhalt der Quelle findenNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Advanced technology for aero gas turbine components. Neuilly sur Seine, France: AGARD, 1987.
Den vollen Inhalt der Quelle findenMasters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Cleveland, Ohio: Lewis Research Center, 1988.
Den vollen Inhalt der Quelle findenJankowsky, 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.
Den vollen Inhalt der Quelle findenJankovsky, 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.
Den vollen Inhalt der Quelle findenFuel rich catalytic combustion, the first stage of a two-stage combustor. [Washington, D.C.]: National Aeronautics and Space Administration, 1985.
Den vollen Inhalt der Quelle findenJ, Przekwas A., und United States. National Aeronautics and Space Administration., Hrsg. Combustion chamber analysis code: Final report. Huntsville, Ala: CFD Research Corp., 1993.
Den vollen Inhalt der Quelle findenCouncil, Coordinating Research, Coordinating Research Council. Performance Committee. und CRC Deposit Group. Combustion Chamber Deposit Program Panel., Hrsg. Combustion chamber deposit research tool development. Alpharetta, Ga: Coordinating Research Council, 2002.
Den vollen Inhalt der Quelle findenCombustion chamber deposit research tool development. Alpharetta, Ga: Coordinating Research Council, 2002.
Den vollen Inhalt der Quelle findenCenter, Lewis Research, Hrsg. Fluids and combustion facility--combustion integrated rack. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Den vollen Inhalt der Quelle findenThe Coenhamworthy Combustion Handbook. CRC Press, 2012.
Den vollen Inhalt der Quelle findenSSME Main Combustion Chamber (MCC) 'hot oil' dewaxing. [Washington, DC: National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenReliability analysis of a structural ceramic combustion chamber. [Washington, DC]: National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenColannino, Joseph. Modeling of Combustion Systems: A Practical Approach. Taylor & Francis Group, 2006.
Den vollen Inhalt der Quelle findenJ, Priem Richard, und United States. National Aeronautics and Space Administration., Hrsg. Analysis of 5 KHz combustion instabilities in 40K methane/LOX combustion chambers. [Washington, DC]: National Aeronautics and Space Administration, 1988.
Den vollen Inhalt der Quelle findenAssociation, National Fire Protection, Hrsg. Boiler and combustion systems hazards code. 2. Aufl. Quincy, MA: National Fire Protection Association, 2004.
Den vollen Inhalt der Quelle findenAssociation, National Fire Protection, Hrsg. Boiler and combustion systems hazards code. 2. Aufl. Quincy, MA: National Fire Protection Association, 2004.
Den vollen Inhalt der Quelle findenAssociation, National Fire Protection, Hrsg. Boiler and combustion systems hazards code. 2. Aufl. Quincy, MA: National Fire Protection Association, 2004.
Den vollen Inhalt der Quelle findenEvans, R. L. Combustion chamber design for a Lean-Burn SI engine. Society of Automotive Engineers., 1992.
Den vollen Inhalt der Quelle finden1926-, Rosenberg S. D., und Lewis Research Center, Hrsg. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. Sacramento, Calif: GenCorp, Aerojet, 1991.
Den vollen Inhalt der Quelle findenHydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. Sacramento, Calif: GenCorp, Aerojet, 1991.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. NASA Lewis Research Center's combustor test facilities and capabilities. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenR, Hicks Yolanda, Hanson Ronald K und United States. National Aeronautics and Space Administration., Hrsg. AST combustion workshop: Working group report. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Den vollen Inhalt der Quelle findenS, Jankovsky Robert, Pavli Albert J und United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., Hrsg. 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.
Den vollen Inhalt der Quelle findenHot 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.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Sacramento, Calif: Aerojet TechSystems, 1990.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., Hrsg. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Sacramento, Calif: Aerojet TechSystems, 1990.
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