Books on the topic 'Gas Turbine Engine Control'

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

C, DeLaat John, and NASA Glenn Research Center, eds. 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, ed. Ceramic thermal barrier coatings for electric utility gas turbine engines. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Center, Lewis Research, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, eds. 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, and United States. National Aeronautics and Space Administration., eds. 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., and United States. Army Aviation Systems Command., eds. Spray automated balancing of rotors: Methods and materials. [Washington, D.C.]: National Aeronautics and Space Administration, 1988.

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

F, Lorenzo Carl, Merrill Walter C, and United States. National Aeronautics and Space Administration., eds. 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, and NASA Glenn Research Center, eds. Wave-rotor-enhanced gas turbine engine demonstrator. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

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

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

E, Welch Gerard, and NASA Glenn Research Center, eds. 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., and NASA Glenn Research Center, eds. High pressure regenerative turbine engine: 21st century propulsion. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

L, Laganelli A., and NASA Glenn Research Center, eds. 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, 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.

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. 3rd ed. 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, and Lewis Research Center, eds. 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.), ed. 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. 2nd ed. [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., ed. Wave rotor demonstrator engine assessment. [Washington, DC]: National Aeronautics and Space Administration, 1996.

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

Engineers, Society of Automotive, and International Fall Fuels & Lubricants Meeting & Exposition (1996 : San Antonio, Tex.), eds. 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, and SAE International Congress & Exposition (1996 : Detroit, Mich.), eds. Engine emissions and emissions measurement. Warrendale, Pa: Society of Automotive Engineers, 1996.

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.