Books on the topic 'Aircraft engine performance'
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North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Comparative engine performance measurements (Mesures comparatives des performances des moteurs). Neuilly-sur-Seine, France: AGARD, 1990.
Find full textFranciscus, Leo C. Supersonic through-flow fan engine and aircraft mission performance. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1989.
Find full textSimon, Donald L. Adaptive optimization of aircraft engine performance using neural networks. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Find full textKobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textKobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textKobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textKobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.
Find full textNeal, Bradford. The implementation and operation of a variable-response electronic throttle control system for a TF-104G aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1989.
Find full textBurkardt, Leo A. General aviation light aircraft propulsion: From the 1940's to the next century. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textMaine, Trindel A. A preliminary evaluation of an F100 engine parameter estimation process using flight data. Moffett Field, Calif: Ames Research Center, 1990.
Find full textSchmidt, D. K. Cooperative control theory and integrated flight and propulsion control: Final technical report for grant NAG3-575 covering the period 1994-1995. College Park, Md: Dept. of Aerospace Engineering, University of Maryland, 1995.
Find full textSymposium, North Atlantic Treaty Organization Advisory Group for Aerospace Research and Development Fluid Dynamics Panel. Aerodynamic engine/airframe integration for high performance aircraft and missiles =: L'intégration aérodynamique des moteurs et des cellules dans les avions et les missiles à hautes performances. Paris: AGARD, 1992.
Find full textWhite, Samuel G. Start up research effort in fluid mechanics: Research project no. 1 : advanced methods for acoustic and thrust benefits for aircraft engine nozzle : performance report-97; performance period: 06/01/96-02/28/97; NASA HQ grant, NAG-1 1835. [Washington, DC: National Aeronautics and Space Administration, 1997.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Aerodynamic engine/airframe integration for high performance aircraft and missiles: Papers presented and discussions held at the Fluid Dynamics Panel Symposium held in Fort Worth, Texas, United States, 7th-10th October 1991. Neuilly-sur-Seine: AGARD, 1992.
Find full textSaravanamuttoo, H. I. H. Recommended practices for measurement of gas path pressures and temperatures for performance assessment of aircraft turbine engines and components. Neuilly sur Seine, France: AGARD, 1990.
Find full textEsker, Barbara S. Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft. [Washington, D.C.]: NASA, 1990.
Find full textTrefny, Charles J. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. Cleveland, Ohio: Lewis Research Center, 1986.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Recommended practices for measurement of gas path pressures and temperatures for performance assessment of aircraft turbine engines and components. Neuilly-sur-Seine: AGARD, 1990.
Find full textNorth Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Recommended practices for the assessment of the effects of atmospheric water ingestion on the performance and operability of gas turbine engines. Neuilly-sur-Seine: AGARD, 1995.
Find full textPerformance study for inlet installations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textCenter, Langley Research, ed. Performance study for inlet installations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.
Find full textJ, Maldonado Jaime, and Lewis Research Center, eds. Supersonic through-flow fan engine and aircrraft mission performance. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1989.
Find full textImproving Algorithmic Efficiency of Aircraft Engine Design for Optimal Mission Performance. Storming Media, 1998.
Find full textUpal, Sengupta, and Dryden Flight Research Facility, eds. The implementation and operation of a variable-response electronic throttle control system for a TF-104G aircraft. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1989.
Find full textGeneral aviation light aircraft propulsion: From the 1940's to the next century. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.
Find full textS, Orme John, Hreha Mark A, and United States. National Aeronautics and Space Administration., eds. Flight test validation of a frequency-based system identification method on an F-15 aircraft. [Washington, DC: National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. Low-order nonlinear dynamic model of IC engine-variable pitch propeller system for general aviation aircraft. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.
Find full textFlight characteristics of the onboard propulsion system model for the performance seeking control algorithm on an F-15 aircraft. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textS, Schkolnik Gerard, and United States. National Aeronautics and Space Administration., eds. Flight characteristics of the onboard propulsion system model for the performance seeking control algorithm on an F-15 aircraft. [Washington, DC]: National Aeronautics and Space Administration, 1995.
Find full textFire suppression system performance of alternative agents in aircraft engine and dry bay laboratory simulations. Gaithersburg, MD: Building and Fire Research Laboratory, National Institute of Standards and Technology, 1995.
Find full textB, Gilyard Glenn, Lambert Heather H, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division., eds. A preliminary evaluation of an F100 engine parameter estimation process using flight data. Washington, D.C: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1990.
Find full textAn experimental and numerical study of icing effects on the performance and controllability of a twin engine aircraft. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1999.
Find full textD, Schierman John, and United States. National Aeronautics and Space Administration., eds. Cooperative control theory and integrated flight and propulsion control: Final report for grant NAG3-998 covering the period 1990-1993. College Park, Md: Dept. of Aerospace Engineering, University of Maryland, 1994.
Find full textF, Borchers Paul, Franklin James A, and Ames Research Center, eds. Moving base simulation of an ASTOVL Lift-fan aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.
Find full textF, Borchers Paul, Franklin James A, and Ames Research Center, eds. Moving base simulation of an ASTOVL Lift-fan aircraft. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1995.
Find full textUnited States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.
Find full textAdvisory Group for Aerospace Research and Development. Fluid Dynamics Panel., ed. Aerodynamic engine/airframe integration for high performance aircraft and missiles: Papers presented and discussions held at the Fluid Dynamics Symposiun held in Fort Worth, Texas, United States, 7th-10th October 1991. Neuilly sur Seine: Agard, 1992.
Find full textCurrent wind tunnel capability and planned improvements at Lewis Research Center. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.
Find full textUnited States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Find full textShock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Find full textUnited States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.
Find full textComputer program for estimating performance of air-breathing aircraft engines. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Division, 1991.
Find full textViper. [Washington, DC: National Aeronautics and Space Administration, 1993.
Find full textUnited States. National Aeronautics and Space Administration., ed. Viper. [Washington, DC: National Aeronautics and Space Administration, 1993.
Find full textT, Norgren Carl, and United States. National Aeronautics and Space Administration., eds. Small gas turbine combustor experimental study: Complaint metal/ceramic liner and performance evaluation. [Washington, DC]: National Aeronautics and Space Administration, 1986.
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