Books on the topic 'Engine thrust'
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United States. National Aeronautics and Space Administration., ed. PPT thrust stand. National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. PPT thrust stand. National Aeronautics and Space Administration, 1995.
Find full textGatlin, Gregory M. Thrust-reverser flow investigation on a twin-engine transport. Langley Research Center, 1988.
Find full textFrank, Quinto P., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Thrust-reverser flow investigation on a twin-engine transport. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Find full textFrank, Quinto P., and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. Thrust-reverser flow investigation on a twin-engine transport. National Aeronautics and Space Administration, Scientific and Technical Information Division, 1989.
Find full textSibtosh, Pal, and NASA Glenn Research Center, eds. Thrust augmentation measurements using a pulse detonation engine ejector. National Aeronautics and Space Administration, Glenn Research Center, 2003.
Find full textRay, Ronald J. Evaluation of various thrust calibration techniques on an F404 engine. Ames Research Center, Dryden Flight Research Facility, 1990.
Find full textNardi Rezende, Rene, ed. Liquid Rocket Engine Thrust Chamber Parametric Modeling. SAE International, 2018. http://dx.doi.org/10.4271/0768093333.
Full textNardi Rezende, Rene. Liquid Rocket Engine Thrust Chamber: Parametrical Modeling. SAE International, 2018. http://dx.doi.org/10.4271/r-465.
Full textHackaday, Gary L. Thrust augmentation for a small turbojet engine. Naval Postgraduate School, 1999.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Evaluation of various thrust calculation techniques on an F404 engine. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Evaluation of various thrust calculation techniques on an F404 engine. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textCenter, Langley Research, ed. High-speed engine/component performance assessment using exergy and thrust-based methods. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textCenter, Langley Research, ed. High-speed engine/component performance assessment using exergy and thrust-based methods. National Aeronautics and Space Administration, Langley Research Center, 1996.
Find full textKacynski, Kenneth J. Thermal stratification potential in rocket engine coolant channels. Lewis Research Center, 1992.
Find full textFacility, Dryden Flight Research, ed. Thrust stand evaluation of engine performance improvement algorithms in an F-15 airplane. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.
Find full textFacility, Dryden Flight Research, ed. Thrust stand evaluation of engine performance improvement algorithms in an F-15 airplane. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.
Find full textHalliwell, Ian. Exoskeletal engine concept: Feasibility studies for medium and small thrust engines [final report]. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textHalliwell, Ian. Exoskeletal engine concept: Feasibility studies for medium and small thrust engines [final report]. National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textJ, Ray Ronald, and Dryden Flight Research Facility, eds. Effects of bleed air extraction on thrust levels of the F404-GE-400 turbofan engine. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.
Find full textAskew, James W. Centaur engine Gimbal friction characteristics under simulated thrust load. National Aeronautics and Space Administration, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. Space transportation booster engine thrust chamber technology: Final report. Aerojet Propulsion Division, 1993.
Find full textR, Conners Timothy, and Dryden Flight Research Facility, eds. Flight evaluation of an extended engine life mode on an F-15 airplane. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.
Find full textR, Conners Timothy, and Dryden Flight Research Facility, eds. Flight evaluation of an extended engine life mode on an F-15 airplane. National Aeronautics and Space Administration, Dryden Flight Research Facility, 1992.
Find full textH, O'Brien C. J., Matthews L. W, and George C. Marshall Space Flight Center., eds. Dual-throat thruster thermal model: Final report. Aerojet TechSystems Co., 1986.
Find full textE, Roschak, and Lewis Research Center, eds. Orbit transfer rocket engine technology: 7.5K-lb thrust rocket engine preliminary design : final report. NASA-Lewis Research Center, 1993.
Find full textW, Burcham Frank, and Dryden Flight Research Facility, eds. Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.
Find full textW, Burcham Frank, and Dryden Flight Research Facility, eds. Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.
Find full textW, Burcham Frank, and Dryden Flight Research Facility, eds. Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.
Find full textMcArdle, Jack G. Outdoor test stand performance of a convertible engine with variable inlet guide vanes for advanced rotorcraft propulsion. National Aeronautics and Space Administration, 1987.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Division., ed. Measurement effects on the calculation of in-flight thrust for an F404 turbofan engine. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1989.
Find full textLeavitt, Laurence D. Static internal performance of a single-engine nonaxisymmetric-nozzle vaned-thrust-reverser design with thrust modulation capabilities. NASA, 1985.
Find full textArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. NASA, 1990.
Find full textArmstrong, Elizabeth S. Cooling of rocket thrust chambers with liquid oxygen. NASA, 1990.
Find full textFacility, Dryden Flight Research, ed. The effect of compressor seventh-stage bleed air extraction on performance of the F100-PW-220 afterburning turbofan engine. National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1991.
Find full textA, Krishnan, Przekwas A. J, and United States. National Aeronautics and Space Administration., eds. Computational analysis of variable thrust engine (VTE) performance: Final report. CFD Research Corp., 1993.
Find full textMacLeod, James D. A derivation of gross thrust for a sea-level jet engine test cell. National Research Council Canada, 1988.
Find full textCenter, Lewis Research, ed. Model engine performance measurement from force balance instrumentation. National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. A simulation evaluation of a four-engine jet transport using engine thrust modulation for flightpath control. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.
Find full textErich, Espenschied, Klop Jeffrey, and United States. National Aeronautics and Space Administration., eds. The control system for the X-33 linear aerospike engine. National Aeronautics and Space Administration, 1998.
Find full textErich, Espenschied, Klop Jeffrey, and United States. National Aeronautics and Space Administration., eds. The control system for the X-33 linear aerospike engine. National Aeronautics and Space Administration, 1998.
Find full textRalph, Sabiers, Schneider Judy, and United States. National Aeronautics and Space Administration., eds. 7.5K lbf thrust engine preliminary design for orbit transfer vehicle: Task D.5 final report. National Aeronautics and Space Administration, 1994.
Find full textRalph, Sabiers, Schneider Judy, and United States. National Aeronautics and Space Administration., eds. 7.5K lbf thrust engine preliminary design for orbit transfer vehicle: Task D.5 final report. National Aeronautics and Space Administration, 1994.
Find full textJohnson, Steven A. A simple dynamic engine model for use in a real-time aircraft simulation with thrust vectoring. National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textUnited States. National Aeronautics and Space Administration., ed. Using engine thrust for emergency flight control: MD-11 and B-747 results. National Aeronautics and Space Administration, 1998.
Find full textW, Burcham Frank, and NASA Dryden Flight Research Center., eds. Using engine thrust for emergency flight control: MD-11 and B-747 results. National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.
Find full textW, Burcham Frank, and NASA Dryden Flight Research Center., eds. Using engine thrust for emergency flight control: MD-11 and B-747 results. National Aeronautics and Space Administration, Dryden Flight Research Center, 1998.
Find full textN, Singnoi Werachone, and United States. National Aeronautics and Space Administration., eds. An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques: Final report. University of Kansas, 1995.
Find full textN, Singnoi Werachone, and United States. National Aeronautics and Space Administration., eds. An analysis of cross-coupling of a multi component jet engine test stand using finite element modeling techniques: Final report. University of Kansas, 1995.
Find full textFacility, Dryden Flight Research, ed. Design, analysis, and control of large transport aircraft utilizing engine thrust as a backup system for the primary flight controls: Semi-annual report in support of grant NAG 2-789. National Aeronautics and Space Administration, Dryden Flight Research Facility, Ames Research Center, 1993.
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