Bücher zum Thema „Combustion chambre“
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Council, Coordinating Research, Coordinating Research Council. Performance Committee., and CRC Deposit Group. Combustion Chamber Deposit Program Panel., eds. Combustion chamber deposit research tool development. Coordinating Research Council, 2002.
Den vollen Inhalt der Quelle findenJ, Przekwas A., and United States. National Aeronautics and Space Administration., eds. Combustion chamber analysis code: Final report. CFD Research Corp., 1993.
Den vollen Inhalt der Quelle findenCenter, Lewis Research, ed. Fluids and combustion facility--combustion integrated rack. National Aeronautics and Space Administration, Lewis Research Center, 1998.
Den vollen Inhalt der Quelle findenQuentmeyer, Richard J. Rocket combustion chamber life-enhancing design concepts. National Aeronautics and Space Administration, Lewis Research Center, 1990.
Den vollen Inhalt der Quelle findenMoon, H. J. Soot generation in a diesel combustion chamber. UMIST, 1996.
Den vollen Inhalt der Quelle findenHu, Tin Cheung John. An experimental and computational investigation of an annular reverse-flow combustor. University of Toronto, 1991.
Den vollen Inhalt der Quelle findenTamaru, Takashi. Hydrogen fueled subsonic-ram-combustor model tests for an air-turbo-ram engine. National Aerospace Laboratory, 1990.
Den vollen Inhalt der Quelle findenShyy, W. A numerical study of flow in gas-turbine combustor. AIAA, 1987.
Den vollen Inhalt der Quelle findenGafurov, R. A. Diagnostika vnutrikamernykh prot͡s︡essov v ėnergeticheskikh ustanovkakh. "Mashinostroenie", 1991.
Den vollen Inhalt der Quelle findenJacobs, P. A. Flow establishment in a generic scramjet combustor. Institute for Computer Applications in Science and Engineering, 1990.
Den vollen Inhalt der Quelle findenAssociation, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. National Fire Protection Association, 2004.
Den vollen Inhalt der Quelle findenAssociation, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. National Fire Protection Association, 2004.
Den vollen Inhalt der Quelle findenAssociation, National Fire Protection, ed. Boiler and combustion systems hazards code. 2nd ed. National Fire Protection Association, 2004.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. NASA Lewis Research Center's combustor test facilities and capabilities. National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenJ, Priem Richard, and United States. National Aeronautics and Space Administration., eds. Analysis of 5 KHz combustion instabilities in 40K methane/LOX combustion chambers. National Aeronautics and Space Administration, 1988.
Den vollen Inhalt der Quelle findenKudinov, Anatoliy, Svetlana Ziganshina, and Kirill Husainov. Calculation of thermal schemes of combined-cycle gas installations of thermal power plants. INFRA-M Academic Publishing LLC., 2023. http://dx.doi.org/10.12737/1865669.
Der volle Inhalt der QuelleBement, David A. Measured operating characteristics of a rectangular combustor/inlet isolator. American Institute of Aeronautics and Astronautics, 1990.
Den vollen Inhalt der Quelle findenColannino, Joseph. Modeling of combustion systems: A practical approach. CRC/Taylor & Francis, 2006.
Den vollen Inhalt der Quelle finden1926-, Rosenberg S. D., and Lewis Research Center, eds. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Final report. GenCorp, Aerojet, 1991.
Den vollen Inhalt der Quelle findenR, Hicks Yolanda, Hanson Ronald K, and United States. National Aeronautics and Space Administration., eds. AST combustion workshop: Working group report. National Aeronautics and Space Administration, 1996.
Den vollen Inhalt der Quelle findenLibbis, N. Coal particle behaviour in a counter-current combustor. Technion Israel Institute of Technology, Dept. of Aeronautical Engineering, 1987.
Den vollen Inhalt der Quelle findenE, 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. National Aeronautics and Space Administration, 1994.
Den vollen Inhalt der Quelle findenC, 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. National Aeronautics and Space Administration ; [St. Louis, Mo.] : US Army Aviation Systems Command, Aviation R&T Activity, 1988.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Aerojet TechSystems, 1990.
Den vollen Inhalt der Quelle findenSyed, Saadat A. Error reduction program: Final report. Lewis Research Center, 1985.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. Hydrocarbon-fuel/combustion-chamber-liner materials compatibility: Interim final report. Aerojet TechSystems, 1990.
Den vollen Inhalt der Quelle findenS, 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. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1992.
Den vollen Inhalt der Quelle findenHoldeman, J. D. A numerical study of the effects of curvature and convergence on dilution jet mixing. National Aeronautics and Space Administration, 1987.
Den vollen Inhalt der Quelle findenL, Lee R. S., Whitelaw James H, Wung T. S, and International Union of Theoretical and Applied Mechanics., eds. Aerothermodynamics in combustors: IUTAM Symposium, Taipei, Taiwan, 1991. Springer-Verlag, 1992.
Den vollen Inhalt der Quelle findenR, Hicks Yolanda, Hanson Ronald K, and United States. National Aeronautics and Space Administration., eds. AST combustion workshop: Diagnostic working group report. National Aeronautics and Space Administration, 1996.
Den vollen Inhalt der Quelle findenShannon, Vinyard, Keribar Rifat, United States. Dept. of Energy. Office of Vehicle and Engine Research and Development., and United States. National Aeronautics and Space Administration., eds. The effect of insulated combustion chamber surfaces on direct-injected diesel engine performance, emissions, and combustion. U.S. Dept. of Energy, Office of Vehicle and Engine R & D, 1989.
Den vollen Inhalt der Quelle findenS, Jankovsky Robert, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Structurally compliant rocket engine combustion chamber: Experimental and analytical validation. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1994.
Den vollen Inhalt der Quelle findenC, Farmer Richard, and United States. National Aeronautics and Space Administration, eds. SSME main combustion chamber and nozzle flowfield analysis: Final report. National Aeronautics and Space Administration, 1986.
Den vollen Inhalt der Quelle findenA, Jeroszko Ronald, Kennedy J. B, and Lewis Research Center, eds. Broad specification fuels combustion technology program, phase II: Final report. Lewis Research Center, National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenUnited States. National Aeronautics and Space Administration., ed. Mixing of multiple jets with a confined subsonic crossflow: Summary of NASA-supported experiments and modeling. National Aeronautics and Space Administration, 1991.
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. National Aeronautics and Space Administration, 1990.
Den vollen Inhalt der Quelle findenHu, T. C. J. An experimental and computational investigation of an annular reverse-flow combustor. Institute for Aerospace Studies, University of Toronto, 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. Springer-Verlag, 1991.
Den vollen Inhalt der Quelle findenA, Winsa Edward, and Lewis Research Center, eds. Fluids and combustion facility--fluid integrated rack. National Aeronautics and Space Administration, Lewis Research Center, 1998.
Den vollen Inhalt der Quelle findenCenter, Langley Research, ed. A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE. National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenCenter, Langley Research, ed. A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE. National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenL, 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. American Institute of Aeronautics and Astronautics, 1996.
Den vollen Inhalt der Quelle findenL, 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. American Institute of Aeronautics and Astronautics, 1996.
Den vollen Inhalt der Quelle findenR, Saunders William, Vandsburger Uri, and NASA Glenn Research Center, eds. A design methodology for rapid implementation of active control systems across lean direct injection combustor platforms. National Aeronautics and Space Administration, Glenn Research Center, 2003.
Den vollen Inhalt der Quelle findenCenter, Langley Research, ed. A two-line absorption instrument for scramjet temperature and water vapor concentration measurement in HYPULSE. National Aeronautics and Space Administration, Langley Research Center, 1998.
Den vollen Inhalt der Quelle findenVecchiarelli, Jack. A proposed combustion chamber for approximating an isothermal heat addition process. National Library of Canada = Bibliothèque nationale du Canada, 1992.
Den vollen Inhalt der Quelle findenC, Ehlers Robert, Parrott Edith, and United States. National Aeronautics and Space Administration., eds. NASA Lewis Research Center's Preheated Combustor and Materials Test Facility. National Aeronautics and Space Administration, 1995.
Den vollen Inhalt der Quelle findenBerger, F. C. Heat transfer from propellant burning in a constant-volume chamber. Department of Aerospace Science and Engineering, University of Toronto, 1990.
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