Книги з теми "Heat engine combustion chamber"
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M, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаM, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаM, Kazaroff John, Jankovsky Robert S, and United States. National Aeronautics and Space Administration., eds. A dual-cooled hydrogen-oxygen rocket engine heat transfer analysis. National Aeronautics and Space Administration, 1991.
Знайти повний текст джерелаA, Roncace Elizabeth, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Hot-gas-side heat transfer characteristics of subscale, plug-nozzle rocket calorimeter chamber. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.
Знайти повний текст джерелаQuentmeyer, Richard J. Hot-gas-side heat transfer characteristics of subscale, plug-nozzle rocket calorimeter chamber. Lewis Research Center, 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Heat transfer in rocket engine combustion chambers and regeneratively cooled nozzles: Final report. SECA, Inc., 1993.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Heat transfer in rocket engine combustion chambers and regeneratively cooled nozzles: Final report. SECA, Inc., 1993.
Знайти повний текст джерелаJankovsky, Robert S. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаD, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаD, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаD, Smith Timothy, Pavli Albert J, and NASA Glenn Research Center, eds. High-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаS, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. National Aeronautics and Spac14., 1988.
Знайти повний текст джерелаMasters, Philip A. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. Lewis Research Center, 1988.
Знайти повний текст джерелаS, Armstrong Elizabeth, Price Harold G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. High-pressure calorimeter chamber tests for liquid oxygen/kerosene (LOX/RP-1) rocket combustion. National Aeronautics and Spac14., 1988.
Знайти повний текст джерелаDon, Hoying, and Universities Space Research Association, eds. Supersonic combustion engine testbed: Heat lightning. Universities Space Research Association, 1990.
Знайти повний текст джерелаS, 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.
Знайти повний текст джерелаBerger, F. C. Heat transfer from propellant burning in a constant-volume chamber. Department of Aerospace Science and Engineering, University of Toronto, 1990.
Знайти повний текст джерелаVecchiarelli, Jack. A proposed combustion chamber for approximating an isothermal heat addition process. National Library of Canada = Bibliothèque nationale du Canada, 1992.
Знайти повний текст джерелаShannon, 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.
Знайти повний текст джерелаWilliam, Brown. Orbit transfer rocket engine technology program: Enhanced heat transfer combustor technology : final report. NASA-Lewis Research Center, 1991.
Знайти повний текст джерелаAmerican Society of Mechanical Engineers. Internal Combustion Engine Division. Technical Conference. New engine technology for cogeneration: Presented at the Internal Combustion Engine Division Technical Conference, Kansas City, Missouri, October 4-7, 1987. American Society of Mechanical Engineers, 1987.
Знайти повний текст джерелаL, Yang S., Schock H. J, Society of Automotive Engineers, and Lewis Research Center, eds. A two-dimensional numerical study of the flow inside the combustion chamber of a motored rotary engine. Society of Automotive Engineers, 1986.
Знайти повний текст джерелаA, Willis Edward, and United States. National Aeronautics and Space Administration., eds. Performance of a supercharged direct-injection stratified-charge rotary combustion engine. NASA, 1990.
Знайти повний текст джерелаBagabir, A. M. Numerical simulation of two-dimensional flow and heat transfer around a hexagonal-shaped combustion chamber. UMIST, 1997.
Знайти повний текст джерелаK, Shaltens Richard, and United States. National Aeronautics and Space Administration., eds. Automotive stirling engine development project. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаCRC Deposit Group. Combustion Chamber Deposit Panel., ed. Literature search on the impact of combustion chamber deposits on engine performance (CRC Project No. CM-136-95). Coordinating Research Council, 1995.
Знайти повний текст джерелаThomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаThomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаThomas, Tomsik, Veres Joseph P, and United States. National Aeronautics and Space Administration., eds. RL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаLee, Nguyen Hung, and United States. National Aeronautics and Space Administration., eds. Performance and efficiency evaluation and heat release study of an outboard marine corporation rotary combustion engine. National Aeronautics and Space Administration, 1987.
Знайти повний текст джерелаRasooli-Nejad, Seyed H. Predictions of heat transfer in a direct-injection diesel engine based on high-speed photographs of combustion. UMIST, 1998.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаMarable, R. W. Design, fabrication, and test of the RL10 derivative II chamber/primary nozzle. Pratt and Whitney Aircraft, 1989.
Знайти повний текст джерелаUnited States. National Aeronautics and Space Administration., ed. Metallized gelled propellants: Oxygen/RP-1/aluminum rocket engine calorimeter heat transfer measurements and analysis. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаCenter, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. Turbine engine hot section technology 1986: Proceedings of a conference. National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.
Знайти повний текст джерелаHeat transfer in rocket engine combustion chambers and regeneratively cooled nozzles. SECA, Inc., 1993.
Знайти повний текст джерелаHeat transfer in rocket engine combustion chambers and regeneratively cooled nozzles. SECA, Inc., 1993.
Знайти повний текст джерелаA Numerical Study of Combined Convective and Radiative Heat Transfer in a Rocket Engine Combustion Chamber. Storming Media, 2002.
Знайти повний текст джерелаNumerical Study of the Effect of the Fuel Film on Heat Transfer in a Rocket Engine Combustion Chamber. Storming Media, 2003.
Знайти повний текст джерелаHigh-area-ratio rocket nozzle at high combustion chamber pressure--experimental and analytical validation. National Aeronautics and Space Administration, Glenn Research Center, 1999.
Знайти повний текст джерелаLederer, Gregor. Rocket Engine on a Student Budget. Technische Universität Dresden, 2021. http://dx.doi.org/10.25368/2022.406.
Повний текст джерелаNational Aeronautics and Space Administration (NASA) Staff. Supersonic Combustion Engine Testbed, Heat Lightning. Independently Published, 2018.
Знайти повний текст джерелаEvans, R. L. Combustion chamber design for a Lean-Burn SI engine. Society of Automotive Engineers., 1992.
Знайти повний текст джерелаSSME Main Combustion Chamber (MCC) 'hot oil' dewaxing. National Aeronautics and Space Administration, 1994.
Знайти повний текст джерелаModeling Engine Spray and Combustion Processes (Heat and Mass Transfer). Springer, 2003.
Знайти повний текст джерелаA two-dimensional numerical study of the flow inside the combustion chamber of a motored rotary engine. Society of Automotive Engineers, 1986.
Знайти повний текст джерелаBusch, Stephen. The Theory and Application of Optical Diagnostic Techniques in the Combustion Chamber of a Diesel Engine. Logos Verlag Berlin, 2013.
Знайти повний текст джерелаDesign Study of Triggered Isomer Heat Exchanger-Combustion Hybrid Jet Engine for High Altitude Flight. Storming Media, 2002.
Знайти повний текст джерелаRL10A-3-3A rocket engine modeling project. National Aeronautics and Space Administration, 1997.
Знайти повний текст джерелаAnalysis of the Application of a Triggered Isomer Heat Exchanger as a Replacement for the Combustion Chamber in an Off-the-Shelf Turbojet. Storming Media, 2001.
Знайти повний текст джерела