Książki na temat „Gas Turbine Engine Control”

D, Southwick Robert, Gallops George W i United States. National Aeronautics and Space Administration., red. High stability engine control (HISTEC). [Washington, DC]: National Aeronautics and Space Administration, 1996.

C, DeLaat John, i NASA Glenn Research Center, red. Active combustion control for aircraft gas turbine engines. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2000.

Lattime, Scott B. Turbine engine clearance control systems: Current practices and future directions. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2002.

Haas, David William. The instrumentation design and control of a T63-A-700 gas turbine engine. Monterey, Calif: Naval Postgraduate School, 1996.

D, Metz Stephen. Survey of gas tubine control for application to marine gas turbine propulsion system control. Monterey, Calif: Naval Postgraduate School, 1989.

Stammettii, Vincent A. Survey and analysis of marine gas turbine control after 1975. Monterey, Calif: Naval Postgraduate School, 1988.

Center, Lewis Research, red. Ceramic thermal barrier coatings for electric utility gas turbine engines. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Center, Lewis Research, i United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, red. Turbine engine hot section technology 1986: Proceedings of a conference. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1986.

Miller, Robert A. Thermal barrier coatings for gas turbine and diesel engines. [Washington, D.C.]: NASA, 1990.

J, Brindley W., Bailey M. Murray i United States. National Aeronautics and Space Administration., red. Thermal barrier coatings for gas turbine and diesel engines. [Washington, D.C.]: NASA, 1990.

Davitt, James A. An evaluation of the potential for expert system application to marine gas turbine control. Monterey, Calif: Naval Postgraduate School, 1988.

Jaw, Link C. Aircraft engine controls: Design, system analysis, and health monitoring. Reston, VA: American Institute of Aeronautics and Astronautics, 2009.

M, Baldwin Richard, Schick Wilbur R, United States. National Aeronautics and Space Administration. i United States. Army Aviation Systems Command., red. Spray automated balancing of rotors: Methods and materials. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

Aircraft gas turbine engine technology. Wyd. 3. New York, N.Y: Glencoe, 1996.

F, Lorenzo Carl, Merrill Walter C i United States. National Aeronautics and Space Administration., red. Screening studies of advanced control concepts for airbreathing engines. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Krueger, Anne O. Xác định tỷ giá hó̂i đoái. Hà Nội: Liên Hiệp công nghệ mới, sản phả̂m mới, 1990.

E, Welch Gerard, i NASA Glenn Research Center, red. Wave-rotor-enhanced gas turbine engine demonstrator. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

E, Welch Gerard, i NASA Glenn Research Center, red. Wave-rotor-enhanced gas turbine engine demonstrator. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

E, Welch Gerard, i NASA Glenn Research Center, red. Wave-rotor-enhanced gas turbine engine demonstrator. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

E, Welch Gerard, i NASA Glenn Research Center, red. Wave-rotor-enhanced gas turbine engine demonstrator. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

Curlett, Brian P. Object-oriented approach for gas turbine engine simulation. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Curlett, Brian P. Object-oriented approach for gas turbine engine simulation. [Washington, DC]: National Aeronautics and Space Administration, 1995.

L, Laganelli A., i NASA Glenn Research Center, red. High pressure regenerative turbine engine: 21st century propulsion. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

L, Laganelli A., i NASA Glenn Research Center, red. High pressure regenerative turbine engine: 21st century propulsion. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

Bennett, J. S. Gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1986.

Kay, Antony L. German jet engine and gas turbine development, 1930-1945. Shrewsbury, England: Airlife, 2002.

Hermsmeyer, Stephan. Improved methods for modelling turbine engine gas flow properties. Birmingham: University of Birmingham, 1996.

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

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

Kuzirian, Robert. Gas turbine systems supervisor. [Pensacola, Fla.]: The Activity, 1994.

Treager, Irwin E. Aircraft gas turbine engine technology: Instructor's manual with transparency masters. Wyd. 3. New York: Glencoe, 1996.

Patnaik, P. C. High temperature protective coatings for aero engine gas turbine components. Ottawa: National Aeronautical Establishment, 1986.

Sankaran, Mahadevan, Tryon Robert G i Lewis Research Center, red. Fatigue reliability of gas turbine engine structures: ... grant NGT-51053. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1997.

Ariffin, A. E. Robust control analysis of a gas-turbine aeroengine. Manchester: UMIST, 1994.

Young, Mark F. Measurements of gas turbine combustor and engine augmentor tube sooting characteristics. Monterey, Calif: Naval Postgraduate School, 1988.

Wallace, William. Methods for crack growth testing in gas turbine engine disc materials. Ottawa: National Aeronautical Establishment, 1987.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Test cases for engine life assessment technology. Neuilly sur Seine, France: AGARD, 1992.

Summers, Robert L. Integrated exhaust gas analysis system for aircraft turbine engine component testing. [Washington, D.C.?]: National Aeronautics and Space Administration, Scientific and Technical Information Branch, 1985.

Wilson, Jack. Optimization of wave rotors for use as gas turbine engine topping cycles. [Washington, DC]: National Aeronautics and Space Administration, 1995.

Naval Education and Training Program Management Support Activity (U.S.), red. Gas turbine system technician (electrical) 3 & 2. [Pensacola, Fla.]: The Activity, 1988.

Gonser, Robert W. Gas turbine system technician (electrical) 3 & 2. [Pensacola, Fla.]: The Activity, 1988.

Garcia, Hector. Testing and development of a shrouded gas turbine engine in a freejet facility. Monterey, Calif: Naval Postgraduate School, 2000.

United States. Environmental Protection Agency. Office of Transportation and Air Quality. Assessment and Standards Division. Nonroad engine growth estimates. Wyd. 2. [Washington, D.C.]: U.S. Environmental Protection Agency, Office of Transportation and Air Quality, Assessment and Standards Division, 2004.

Hanley, David. Advanced high temperature polymer matrix composites for gas turbine engines program expansion. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

United States. National Aeronautics and Space Administration., red. Wave rotor demonstrator engine assessment. [Washington, DC]: National Aeronautics and Space Administration, 1996.

United States. National Aeronautics and Space Administration., red. Wave rotor demonstrator engine assessment. [Washington, DC]: National Aeronautics and Space Administration, 1996.

Engineers, Society of Automotive, i International Fall Fuels & Lubricants Meeting & Exposition (1996 : San Antonio, Tex.), red. Diesel engine combustion and emission control. Warrendale, PA: Society of Automotive Engineers, 1996.

Davitt, James A. A baseline expert control system for marine gas turbine compressor surge. Monterey, California: Naval Postgraduate School, 1989.

Engineers, Society of Automotive, i SAE International Congress & Exposition (1996 : Detroit, Mich.), red. Engine emissions and emissions measurement. Warrendale, Pa: Society of Automotive Engineers, 1996.

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