Книги з теми "Aircraft engine performance"

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.

Franciscus, Leo C. Supersonic through-flow fan engine and aircraft mission performance. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1989.

Simon, Donald L. Adaptive optimization of aircraft engine performance using neural networks. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

Kobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Kobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Kobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Kobayashi, Takahisa. A hybrid neural network-genetic algorithm technique for aircraft engine performance diagnostics. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Neal, 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.

Burkardt, 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.

Maine, Trindel A. A preliminary evaluation of an F100 engine parameter estimation process using flight data. Moffett Field, Calif: Ames Research Center, 1990.

Schmidt, 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.

Symposium, 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.

White, 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.

North 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.

Saravanamuttoo, 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.

Esker, Barbara S. Performance characteristics of a one-third-scale, vectorable ventral nozzle for SSTOVL aircraft. [Washington, D.C.]: NASA, 1990.

Trefny, Charles J. Low-speed performance of an axisymmetric, mixed-compression, supersonic inlet with auxiliary inlets. Cleveland, Ohio: Lewis Research Center, 1986.

North 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.

North 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.

Performance study for inlet installations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

Center, Langley Research, ed. Performance study for inlet installations. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1992.

J, 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.

Improving Algorithmic Efficiency of Aircraft Engine Design for Optimal Mission Performance. Storming Media, 1998.

Upal, 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.

General aviation light aircraft propulsion: From the 1940's to the next century. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

S, 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.

United 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.

United 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.

United 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.

United 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.

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.

S, 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.

Fire 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.

B, 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.

An 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.

D, 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.

F, 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.

F, 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.

United States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration., ed. NASA Lewis Propulsion Systems Laboratory customer guide manual. [Washington, DC]: National Aeronautics and Space Administration, 1994.

Advisory 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.

Current wind tunnel capability and planned improvements at Lewis Research Center. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

United States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.

Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.

United States. National Aeronautics and Space Administration., ed. Shock-tunnel combustor testing for hypersonic vehicles. San Jose, Calif: MCAT Institute, 1994.

Computer 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.

Viper. [Washington, DC: National Aeronautics and Space Administration, 1993.

United States. National Aeronautics and Space Administration., ed. Viper. [Washington, DC: National Aeronautics and Space Administration, 1993.

T, 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.