Books on the topic 'Turbine propeller engines'

United States. National Aeronautics and Space Administration., ed. Large-scale advanced prop-fan (LAP): Final report. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies, 1988.

United States. National Aeronautics and Space Administration., ed. Large-scale advanced prop-fan (LAP): Final report. [Windsor Locks, CT]: Hamilton Standard Division, United Technologies, 1988.

Danielle, DiCicco L., Nowlin Brent C, and United States. National Aeronautics and Space Administration., eds. Experimental evaluation of a cooled radial-inflow turbine. [Washington, DC]: National Aeronautics and Space Administration, 1993.

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

Levin, Alan D. Aerodynamic and propeller performance characteristics of a propfan-powered, semispan model. Moffett Field, Calif: National Aeronautics and Space Administration, Ames Research Center, 1988.

Anderson, R. D. Advanced propfan engine technology (APET) definition study, single and counter-rotation gearbox/pitch change mechanism design. [Washington, DC: National Aeronautics and Space Administration, 1987.

Patterson, James C. Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Patterson, James C. Evaluation of installed performance of a wing-tip-mounted pusher turboprop on a semispan wing. [Washington, D.C.]: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1987.

Whitlow, John B. NASA advanced turboprop research and concept validation program. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Center, Lewis Research, ed. Energy efficient engine high-pressure turbine component rig performance test report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

G, Ludemann S., and Lewis Research Center, eds. Large-scale advanced propfan (LAP) program progress report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

United States. National Aeronautics and Space Administration., ed. Full scale technology demonstration of a modern counterrotating unducted fan engine concept. [Washington, DC]: National Aeronautics and Space Administration, 1989.

A, Yokel S., and United States. National Aeronautics and Space Administration., eds. PMR graphite engine duct development: Final report. [Washington, DC]: National Aeronautics and Space Administration, 1989.

G, Ludemann S., and Lewis Research Center, eds. Large-scale advanced propfan (LAP) program progress report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

United States. Army Aviation Research and Technology Activity. and United States. National Aeronautics and Space Administration., eds. Effects of inlet distortion on the development of secondary flows in a subsonic axial inlet compressor rotor. [Washington, DC]: National Aeronautics and Space Administration, 1991.

B, Whitlow John, and United States. National Aeronautics and Space Administration., eds. NASA/industry advanced turboprop technology program. [Washington, DC]: National Aeronautics and Space Administration, 1988.

United States. National Aeronautics and Space Administration., ed. Advanced prop-fan engine technology (APET) single- and counter-rotation gearbox/pitch change mechanism: Final report. [Washington, DC: National Aeronautics and Space Administration, 1985.

United States. National Aeronautics and Space Administration., ed. Advanced propfan engine technology (APET) and single-rotation gearbox/pitch change mechanism. [Washington, DC: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., ed. Advanced propfan analysis for the family of commuter airplanes. [Washington, DC: National Aeronautics and Space Administration, 1987.

W, Niedzwiecki Richard, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. An overview of the small engine component technology (SECT) studies. [Washington, DC]: National Aeronautics and Space Administration, 1986.

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.

General Electric Company. GE36 Project Dept. and United States. National Aeronautics and Space Administration., eds. Full scale technology demonstration of a modern counterrotating unducted fan engine concept: Design report. [Washington, D.C.]: National Aeronautics and Space Administration, 1989.

G, Ludemann S., and Lewis Research Center, eds. Large-scale advanced propfan (LAP) program progress report. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1985.

United States. National Aeronautics and Space Administration., ed. Advanced prop-fan engine technology (APET) single- and counter rotation gearbox/pitch change mechanism: Final report. [Washington, DC: National Aeronautics and Space Administration, 1987.

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.

United States. National Aeronautics and Space Administration., ed. Effects of turbine cooling assumptions on performance and sizing of high-speed civil transport. [Washington, DC]: National Aeronautics and Space Administration, 1992.

1937-, Scott James R., and United States. National Aeronautics and Space Administration., eds. Coupled aerodynamic and acoustical predictions for turboprops. [Washington, DC]: National Aeronautics and Space Administration, 1987.

E, Rose Gayle, Podboy Gary G, and United States. National Aeronautics and Space Administration., eds. Wind tunnel performance results of an aeroelastically scaled 2/9 model of the PTA flight test prop-fan. [Washington, DC]: National Aeronautics and Space Administration, 1987.

Rosen, Robert. The Future challenge for aeropropulsion. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1992.

Plencner, Robert M. Plotting component maps in the Navy/NASA Engine Program (NNEP): A method and its usage. [Washington, DC]: National Aeronautics and Space Administration, 1989.

L, Braslow Albert, Butterfield A. J, and Langley Research Center, eds. Circulation control propellers for general aviation, including a BASIC computer program. Hampton, Va: National Aeronautics and Space Administration, Langley Research Center, 1985.

V, Sundt C., McKibbon A. H, and United States. National Aeronautics and Space Administration., eds. Advanced gearbox technology: Advanced counter-rotating gearbox : detailed design report. [Washington, DC]: National Aeronautics and Space Administration, 1988.

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. [Washington, DC: National Aeronautics and Space Administration, 1993.

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. [Washington, DC: National Aeronautics and Space Administration, 1993.

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. [Washington, DC: National Aeronautics and Space Administration, 1993.

J, Loeffler Irvin, and United States. National Aeronautics and Space Administration., eds. In-flight near- and far-field acoustic data measured on the propfan test assessment (PTA) testbed and with an adjacent aircraft. [Washington, DC: National Aeronautics and Space Administration, 1993.

Kay, Antony L. Turbojet: History and development. Ramsbury: Crowood, 2007.

Hager, Roy D. Advanced turboprop project. Washington, DC: Scientific and Technical Information Division, National Aeronautics and Space Administration, 1988.

Hancock, J. P. Analysis of results from wind tunnel tests of inlets for an advanced turboprop nacelle installation. [Washington, DC]: National Aeronautics and Space Administration, 1989.

United States. National Aeronautics and Space Administration., ed. Test stand performance of a convertible engine for advance V/STOL and rotorcraft propulsion. [Washington, DC?: National Aeronautics and Space Administration, 1987.

United States. National Aeronautics and Space Administration., ed. Potential reduction of en route noise from an advanced turboprop aircraft. [Washington, DC]: National Aeronautics and Space Administration, 1990.

Hager, Roy D. Advanced turboprop project. Washington, D.C: Scientific and Technical Information Division, National Aeronautics and Space Administration, 1988.

V, Kaza K. R., and United States. National Aeronautics and Space Administration., eds. Concentrated mass effects on the flutter of a composite advanced turboprop model. [Washington, DC]: National Aeronautics and Space Administration, 1987.

Deborah, Vrabel, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Division, eds. Advanced turboprop project. Washington, DC: Scientific and Technical Information Division, National Aeronautics and Space Administration, 1988.

Chandrashekar, S. Technology & innovation in China: A case study of single crystal superalloy development for aircraft turbine blades. Bangalore: International Strategic & Security Studies Programme, National Institute of Advanced Studies, 2011.

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.

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): Programmer's manual. [Washington, DC]: National Aeronautics and Space Administration, 1989.

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): Theoretical manual. [Washington, DC]: National Aeronautics and Space Administration, 1992.

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): User's manual. [Washington, DC]: National Aeronautics and Space Administration, 1991.

Brown, K. W. Structural Tailoring of Advanced Turboprops (STAT): Interim report. [Cleveland, Ohio]: National Aeronautics and Space Administration, 1988.