Books on the topic 'Heat-transfer; Aerospace gas turbines'

Garg, Vijay K. Heat transfer in gas turbines. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

North Atlantic Treaty Organization. Advisory Group for Aerospace Research and Development. Heat Transfer and Cooling in Gas Turbines. S.l: s.n, 1985.

Meeting, American Society of Mechanical Engineers Winter. Heat transfer in gas turbine engines. New York, N.Y. (345 E. 47th St., New York 10017): The Society, 1987.

1953-, Dutta Sandip, and Ekkad Srinath 1958-, eds. Gas turbine heat transfer and cooling technology. New York: Taylor & Francis, 2000.

International Symposium on Heat Transfer in Turbomachinery (1992 Marathon, Greece). Heat transfer in turbomachinery: Proceedings of the International Symposium on Heat Transfer the (sic) in Turbomachinery, Greece, August 1992. New York: Begell House, 1994.

Sandīpa, Datta, and Ekkad Srinath 1958-, eds. Gas turbine heat transfer and cooling technology. 2nd ed. Boca Raton, FL: Taylor & Francis, 2012.

American Society of Mechanical Engineers. Heat transfer in gas turbine engines and three-dimensional flows. New York: American Society of Mechanical Engineers, 1988.

American Society of Mechanical Engineers. Winter Meeting. Heat transfer in gas turbine engines - 1991: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Atlanta, Georgia, December 1-6, 1991. New York, N.Y: ASME, 1991.

Ameri, A. A. Analysis of gas turbine rotor blade tip and shroud heat transfer. [Washington, DC: National Aeronautics and Space Administration, 1996.

Ameri, A. A. Analysis of gas turbine rotor blade tip and shroud heat transfer. [Washington, DC: National Aeronautics and Space Administration, 1998.

American Society of Mechanical Engineers. Winter Meeting. Fundamental and applied heat transfer research for gas turbine engines: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Anaheim, California, November 8-13, 1992. New York, N.Y: American Society of Mechanical Engineers, 1992.

Boyle, Robert J. Prediction of nonuniform inlet temperature effects on vane and rotor heat transfer. [Washington, D.C: National Aeronautics and Space Administration, 1997.

American Society of Mechanical Engineers. Winter Meeting. Heat transfer in gas turbine engines and three-dimensional flows: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Chicago, Illinois, November 27-December 2, 1988. New York, N.Y. (United Engineering Center, 345 E. 47th St., New York 10017): The Society, 1988.

Graham, Robert W. Recent progress in research pertaining to estimates of gas-side heat transfer in an aircraft gas turbine. [Washington, D.C.]: NASA, 1990.

Symposium of the AGARD Propulsion and Energetics Panel (65th 1985 Bergen, Norway). Heat transfer and cooling in gas turbines: Papers presented at the Propulsion and Energetics Panel 65th Symposium, held in Bergen, Norway, 6-10 May 1985. Neuilly sur Seine, France: North Atlantic Treaty Organization, Advisory Group for Aerospace Research and Development, 1985.

Bartnik, Ryszard. The Modernization Potential of Gas Turbines in the Coal-Fired Power Industry: Thermal and Economic Effectiveness. London: Springer London, 2013.

Advisory Group for Aerospace Research and Development. Propulsion and Energetics Panel. Symposium. Heat transfer and cooling in gas turbines: Papers presented at the Propulsion and Energetics Panel 65th symposium held in Bergen, Norway, 6-10 May 1985. Neuilly sur Seine: Agard, 1985.

Center, NASA Glenn Research, ed. Heat transfer in gas turbines. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2001.

(Editor), Bengt Sunden, and Mohammad Faghri (Editor), eds. Heat Transfer in Gas Turbines. Wit Pr/Computational Mechanics, 2001.

M, McEligot Donald, American Society of Mechanical Engineers. Heat Transfer Division., and National Heat Transfer Conference (29th : 1993 : Atlanta, Ga.), eds. Gas turbine heat transfer, 1993: Presented at the 29th National Heat Transfer Conference, Atlanta, Georgia, August 8-11, 1993. New York: American Society of Mechanical Engineers, 1993.

Asme Turbo Expo: Heat Transfer, Transition, Internal Air and Seals. American Society of Mechanical Engineers, 2004.

Heat transfer and cooling in gas turbines: Papers presented at the Propulsion and Energetics Panel 80th Symposium held in Antalya, Turkey, 12th-16th October 1992. Neuilly-sur-Seine, France: AGARD, 1993.

K, Chyu M., Nirmalan N. V, American Society of Mechanical Engineers. Heat Transfer Division., and International Mechanical Engineering Congress and Exposition (1994 : Chicago, Ill.), eds. Heat transfer in gas turbines: Presented at 1994 International Mechanical Engineering Congress and Exposition, Chicago, Illinois, November 6-11, 1994. New York: American Society of Mechanical Engineers, 1994.

A, Hippensteele Steven, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Vidualization techniques to experimentally model flow and heat transfer in turbine and aircraft flow passages. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1991.

Ga.) International Mechanical Engineering Congress and Exposition (1996 : Atlanta. Heat Transfer in Gas Turbines: Presented at 1994 International Mechanical Engineering Congress and Exposition, Chicago, Illinois, November 6-11, 1994 (Htd (Series), V. 300.). American Society of Mechanical Engineers, 1994.

E, Elovic, Martin H. L. 1949-, American Society of Mechanical Engineers. Winter Meeting, and American Society of Mechanical Engineers. Heat Transfer Division., eds. Heat transfer in gas turbine engines, 1991: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, Atlanta, Georgia, December 1-6, 1991. New York: The Society, 1991.

C, Han J., Mayle R. E, American Society of Mechanical Engineers. Heat Transfer Division., and American Society of Mechanical Engineers. Winter Meeting, eds. Heat transfer in gas turbine engines: Presented at the Winter Annual Meeting of the American Society of Mechanical Engineers, San Francisco, California, December 10-15, 1989. New York, N.Y: American Society of Mechanical Engineers, 1989.

Heat transfer and flow on the first stage blade tip of a power generation gas turbine. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

E, Steinthorsson, Rigby David L, and Lewis Research Center, eds. Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

Effects of tip clearance and casing recess on heat transfer and stage efficiency in axial turbines. [Cleveland, Ohio]: National Aeronautics and Space Administration, Lewis Research Center, 1998.

S, Bunker Ronald, and NASA Glenn Research Center, eds. Augmentation of stagnation region heat transfer due to turbulence from a DLN can combustor. Cleveland, Ohio: National Aeronautics and Space Administration, Glenn Research Center, 2000.

Prediction of film cooling on gas turbine airfoils. [Washington, DC]: National Aeronautics and Space Administration, 1994.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Experimental study of vane heat transfer and film cooling at elevated levels of turbulence. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., ed. Experimental study of vane heat transfer and film cooling at elevated levels of turbulence. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1996.

Bartnik, Ryszard. The Modernization Potential of Gas Turbines in the Coal-Fired Power Industry: Thermal and Economic Effectiveness. Springer, 2013.

R, Chen, Cline M. C, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

R, Chen, Cline M. C, and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

L, Yang S., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

L, Yang S., and United States. National Aeronautics and Space Administration., eds. Numerical simulation of a low emissions gas turbine combustor using KIVA-II. [Washington, DC: National Aeronautics and Space Administration, 1996.

S, Samuelsen G., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing in a reacting cylindrical crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

United States. National Aeronautics and Space Administration., ed. Composite matrix experimental combustor: Final technical report. [Washington, D.C.]: NASA, 1994.

S, Samuelsen G., Holdeman J. D, and United States. National Aeronautics and Space Administration., eds. Jet mixing in a reacting cylindrical crossflow. [Washington, DC]: National Aeronautics and Space Administration, 1995.

The effects of Reynolds number, motor incidence angle and surface roughness on the heat transfer distribution in a large-scale turbine rotor passage. East Hartford, Conn: United Technologies Research Center, 1991.

M, Tomsik Thomas, and United States. National Aeronautics and Space Administration., eds. Prediction of the ullage gas thermal stratification in a NASP vehicle propellant tank experimental simulation using FLOW-3D. [Washington, D.C.]: NASA, 1990.

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.