Books on the topic 'Turbine blade'

Ghodke, Chaitanya D. Gas Turbine Blade Cooling. Warrendale, PA: SAE International, 2018. http://dx.doi.org/10.4271/0768095069.

Ghodke, Chaitanya. Gas Turbine Blade Cooling. Warrendale, PA: SAE International, 2018. http://dx.doi.org/10.4271/pt-196.

Shea, Daniel. Ceramic barrier turbine blade demonstration. Watertown, Massachusetts: U.S.Army Materials Technology Laboratory, 1986.

Zhang, Dinghua, Yunyong Cheng, Ruisong Jiang, and Neng Wan. Turbine Blade Investment Casting Die Technology. Berlin, Heidelberg: Springer Berlin Heidelberg, 2018. http://dx.doi.org/10.1007/978-3-662-54188-3.

P, Camperchioli William, López Freyle Isaac, United States. Army Aviation Systems Command., and United States. National Aeronautics and Space Administration., eds. Transonic turbine blade cascade testing facility. [Washington, DC: National Aeronautics and Space Administration, 1992.

Noot, Marc. Numerical analysis of turbine blade cooling ducts. Eindhoven: Eindhoven University, 1997.

Baumeister, Kenneth J. Unsteady heat transfer in turbine blade ducts. [Washington, DC]: National Aeronautics and Space Administration, 1988.

Martinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

Martinez-Sanchez, Manuel. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

M, Greitzer Edward, George C. Marshall Space Flight Center., and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

M, Greitzer Edward, George C. Marshall Space Flight Center, and Massachusetts Institute of Technology, eds. Turbine blade-tip clearance excitation forces: Final report on Contract number NAS8-35018. Cambridge, Mass: Massachusetts Institute of Technology, 1985.

Boyle, Robert J. Navier-Stokes analysis of turbine blade heat transfer. [Washington, D.C.]: NASA, 1990.

Boyle, Robert J. Navier-Stokes analysis of turbine blade heat transfer. [Washington, D.C.]: NASA, 1990.

Boyle, Robert J. Navier-Stokes analysis of turbine blade heat transfer. [Washington, D.C.]: NASA, 1990.

Boyle, Robert J. Navier-Stokes analysis of turbine blade heat transfer. [Washington, D.C.]: NASA, 1990.

Lio, Wai Hou. Blade-Pitch Control for Wind Turbine Load Reductions. Cham: Springer International Publishing, 2018. http://dx.doi.org/10.1007/978-3-319-75532-8.

Liebert, Curt H. Heat flux measurement in SSME turbine blade tester. [Washington, DC]: National Aeronautics and Space Administration, 1990.

R, Black Gerald, and Lewis Research Center, eds. [Blade loss transient dynamics analysis.: Final report]. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

C, Gallardo V., and Lewis Research Center, eds. [Blade loss transient dynamics analysis.: Final report]. [Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1986.

Klima, Stanley J. NDE of PWA 1480 single crystal turbine blade material. [Washington, DC: National Aeronautics and Space Administration, 1993.

A, Davis Gary. Blade tip rubbing stress prediction: Final report. Canoga Park, Calif: Rockwell International, Rocketdyne Division, 1991.

E, Steinthorsson, and United States. National Aeronautics and Space Administration., eds. Prediction of unshrouded rotor blade tip heat transfer: Under cooperative agreement NCC3-370. [Washington, DC: National Aeronautics and Space Administration, 1994.

A, Cyr M., Strange R. R, and United States. National Aeronautics and Space Administration., eds. Turbine blade and vane heat flux sensor development phase 2. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Garg, Vijay Kumar. Leading edge film cooling effects on turbine blade heat transfer. [Washington, DC]: National Aeronautics and Space Administration, 1995.

A, Cyr M., Strange R. R, and United States. National Aeronautics and Space Administration, eds. Turbine blade and vane heat flux sensor development phase 2. [Washington, DC]: National Aeronautics and Space Administration, 1985.

Waite, Anthony Richard. The application of robotics to the turbine blade encapsulation process. Birmingham: Aston University. Interdisciplinary Higher Degrees Scheme, 1987.

Ltd, Nor'wester Energy Systems. Wind turbine rotor blade contamination and effects on performance: A study. Ottawa: The Branch, 1989.

Fitting, Dale W. High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction. Boulder, Colo: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1998.

P, Dubé W., Siewert T. A, and National Institute of Standards and Technology (U.S.), eds. High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction. Boulder, Colo: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1998.

P, Dubé W., Siewert T. A, and National Institute of Standards and Technology (U.S.), eds. High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction. Boulder, Colo: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1998.

Fitting, Dale W. High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction. Boulder, Colo: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1998.

Fitting, Dale W. High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction. Boulder, Colo: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1998.

Fitting, Dale W. High-energy, transmission X-ray diffraction for monitoring turbine-blade solidifaction. Boulder, Colo: U.S. Dept. of Commerce, Technology Administration, National Institute of Standards and Technology, 1998.

Boyle, Robert J. Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows. [Washington, D.C.]: NASA, 1992.

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

Lee, Henry. Space shuttle main engine high pressure fuel turbopump turbine blade cracking. [Marshall Space Flight Center, Ala.?]: National Aeronautics and Space Administration, George C. Marshall Space Flight Center, 1988.

Abdul-Aziz, Ali. Thermal finite-element analysis of space shutle main engine turbine blade. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

W, Giel P., and NASA Glenn Research Center, eds. Blade heat transfer measurements and predictions in a transonic turbine cascade. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 1999.

T, Tong Michael, Kaufman Albert 1928-, and Lewis Research Center, eds. Thermal finite-element analysis of space shutle main engine turbine blade. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

Arts, T. Three dimensional rotational inviscid flow calculation in axial turbine blade rows. Rhode Saint Genese, Belgium: Von Karman Institute, 1985.

Boyle, Robert J. Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows. [Washington, D.C.]: NASA, 1992.

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

Boyle, Robert J. Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows. [Washington, D.C.]: NASA, 1992.

Arts, Tony. Three dimensional rotational inviscid flow calculation in axial turbine blade rows. Rhode Saint Genese, Belgium: von Karman Institute for Fluid Dynamics, 1985.

Boyle, Robert J. Three-dimensional Navier-Stokes heat transfer predictions for turbine blade rows. [Washington, D.C.]: NASA, 1992.

Abdul-Aziz, Ali. Thermal finite-element analysis of space shutle main engine turbine blade. Cleveland, Ohio: National Aeronautics and Space Administration, Lewis Research Center, 1987.

Kypuros, Javier A. A reduced model for prediction of thermal and rotational effects on turbine tip clearance. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

J, Melcher Kevin, and NASA Glenn Research Center, eds. A reduced model for prediction of thermal and rotational effects on turbine tip clearance. [Cleveland, Ohio]: National Aeronautics and Space Administration, Glenn Research Center, 2003.

L, Dreshfield Robert, and United States. National Aeronautics and Space Administration., eds. Progress toward a tungsten alloy wire/high temperature alloy composite turbine blade. [Washington, DC: National Aeronautics and Space Administration, 1992.

L, Dreshfield Robert, and United States. National Aeronautics and Space Administration., eds. Progress toward a tungsten alloy wire/high temperature alloy composite turbine blade. [Washington, DC: National Aeronautics and Space Administration, 1992.