Books on the topic 'Turbofan engines'

Richter, Hanz. Advanced Control of Turbofan Engines. New York, NY: Springer New York, 2012. http://dx.doi.org/10.1007/978-1-4614-1171-0.

Richter, Hanz. Advanced control of turbofan engines. New York, NY: Springer, 2012.

Meyer, Harold D. Aeroacoustic analysis of turbofan noise generation. Cleveland, Ohio: Lewis Reserch Center, 1996.

A, Kirchgessner Thomas, and United States. National Aeronautics and Space Administration., eds. Airflow calibration and exhaust pressure temperature survey of an F-404, S/N 215-209, turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1987.

Hang kong wo lun feng shan fa dong ji. [Peking]: Guo fang gong ye chu ban she, 1985.

Christopher, Snyder, Knip Gerald, and United States. National Aeronautics and Space Administration., eds. Advanced core technology: Key to subsonic propulsion benefits. [Washington, DC]: National Aeronautics and Space Administration, 1989.

A, Wynosky T., and United States. National Aeronautics and Space Administration., eds. Energy efficient engine program: Advanced turbofan nacelle definition study. [Washington, DC: National Aeronautics and Space Administration, 1985.

Litt, John. A real-time simulator of a turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1989.

C, DeLaat John, Merrill Walter C, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. A real-time simulator of a turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1989.

C, DeLaat John, Merrill Walter C, United States. Army Aviation Research and Technology Activity., and United States. National Aeronautics and Space Administration., eds. A real-time simulator of a turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Hill, Philip G. An educational introduction to transonic compressor stage design principles. Warrendale, Pa: Society of Automotive Engineers, 1993.

Tavares, T. S. A supersonic fan equipped variable cycle engine for a Mach 2.7 supersonic transport. Cleveland, Ohio: Lewis Research Center, 1985.

W, Premo John, Hersh Alan S, Langley Research Center, and United States. National Aeronautics and Space Administration., eds. Advanced turbofan duct liner concepts. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1999.

L, Simon Donald, and NASA Glenn Research Center, eds. Kalman filtering with inequality constraints for turbofan engine health estimation. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

Litt, John. A microprocessor-based real-time simulator of a turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1988.

C, DeLaat John, Merrill Walter C, United States. National Aeronautics and Space Administration., and United States. Army Aviation Research and Technology Activity., eds. A microprocessor-based real-time simulator of a turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1988.

FEDERAL AVIATION ADMINISTRATION. Type certification basis for conversion from reciprocating engine to turbine engine-powered part 23 airplanes. Washington, D.C. (800 Independence Ave., S.W., (Washington 20591): U.S. Dept. of Transportation, Federal Aviation Administration, 1993.

United States. National Aeronautics and Space Administration., ed. A linear control design structure to maintain loop properties during limit operation in a multi-nozzle turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1991.

United States. National Aeronautics and Space Administration., ed. HYTESS II, a hypothetical turbofan engine simplified simulation with multivariable control and sensor analytical redundancy. [Washington, DC]: National Aeronautics and Space Administration, 1986.

W, Burcham Frank, and Dryden Flight Research Facility, eds. Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.

Fanelli, Frank. R/C ducted fans: How to build and fly your own jet successfully. Osceola, Wis: Motorbooks International, 1987.

W, Burcham Frank, and Dryden Flight Research Facility, eds. Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.

United States. National Aeronautics and Space Administration., ed. A linear control design structure to maintain loop properties during limit operation in a multi-nozzle turbofan engine. [Washington, DC]: National Aeronautics and Space Administration, 1991.

W, Burcham Frank, and Dryden Flight Research Facility, eds. Exhaust-gas pressure and temperature survey of F404-GE-400 turbofan engine. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1988.

T, Brown Steven, Kawai Ron T, and NASA Glenn Research Center, eds. Ultra-efficient engine diameter study. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

T, Brown Steven, Kawai Ron T, and NASA Glenn Research Center, eds. Ultra-efficient engine diameter study. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

Drummond, Colin K. Real-time simulation of an F110/STOVL turbofan engine. [Washington, D.C.]: NASA, 1989.

J, Ouzts Peter, and United States. National Aeronautics and Space Administration., eds. Real-time simulation of an F110/STOVL turbofan engine. [Washington, D.C.]: NASA, 1989.

Linke-Diesinger, Andreas. Systems of Commercial Turbofan Engines: An Introduction to Systems Functions. Berlin, Heidelberg: Springer-Verlag, 2008.

M, Jones Scott, Paxson Daniel E, and United States. National Aeronautics and Space Administration., eds. Wave rotor-enhanced gas turbine engines. [Washington, DC]: National Aeronautics and Space Administration, 1995.

M, Jones Scott, Paxson Daniel E, and United States. National Aeronautics and Space Administration., eds. Wave rotor-enhanced gas turbine engines. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Garg, Sanjay. Turbofan engine control system design using the LQG/LTR methodology. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

Facility, Dryden Flight Research, ed. A simulation study of turbofan engine deterioration estimation using Kalman filtering techniques. Edwards, Calif: National Aeronautics and Space Administration, Ames Research Center, Dryden Flight Research Facility, 1991.

Balepin, Vladimir. NOx emission reduction in commercial jets through water injection. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

C, DeLaat John, Bruton William M, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Advanced detection, isolation, and accomodation of sensor failures, real-time evaluation. [Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

C, DeLaat John, Bruton William M, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Office., eds. Advanced detection, isolation, and accomodation of sensor failures, real-time evaluation. [Washington, D.C: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Halliwell, Ian. Exoskeletal engine concept: Feasibility studies for medium and small thrust engines [final report]. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Halliwell, Ian. Exoskeletal engine concept: Feasibility studies for medium and small thrust engines [final report]. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Miller, Max J. Small Engine Technology (SET): Task 14, axisymmetric engine simulation environment, draft final report. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. On the estimation algorithm used in adaptive performance optimization of turbofan engines. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program, ed. On the estimation algorithm used in adaptive performance optimization of turbofan engines. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1993.

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.

Wake, L. V. Investigation of coating performance and corrosion of compressor components in the TF30-P-3 engine of F111C aircraft. Ascot Vale, Vic: Materials Research Laboratories, 1986.

Sanjay, Garg, and United States. National Aeronautics and Space Administration., eds. A comparison of multivariable control design techniques for a turbofan engine control. [Washington, D.C.]: National Aeronautics and Space Administration, 1995.

P, Woodward Richard, and United States. National Aeronautics and Space Administration., eds. Noise levels from a model turbofan engine with simulated noise control measures applied. [Washington, DC: National Aeronautics and Space Administration, 1993.

Center, NASA Glenn Research, ed. Source methodology for turbofan noise prediction (SOURCED3D technical documentation). [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

G, Sofrin T., and United States. National Aeronautics and Space Administration., eds. Method for extracting forward acoustic wave components from rotating microphone measurements in the inlets of turbofan engines. [Washington, DC]: National Aeronautics and Space Administration, 1995.