Books on the topic 'Axial flow impeller blades'
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Consult the top 17 books for your research on the topic 'Axial flow impeller blades.'
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Arts, T. Three dimensional rotational inviscid flow calculation in axial turbine blade rows. Rhode Saint Genese, Belgium: Von Karman Institute, 1985.
Find full textNeuhoff, F. Modifications to the inlet flow field of a transonic compressor rotor. Monterey, Calif: Naval Postgraduate School, 1985.
Find full textArasu, A. Valan. Turbo machines. New Delhi: Vikas Publishing House, 2008.
Find full textWasserbauer, Charles A. NASA low-speed axial compressor for fundamental research. Cleveland, Ohio: Lewis Research Center, 1995.
Find full textEscudier, Marcel. Flow through axial-flow-turbomachinery blading. Oxford University Press, 2018. http://dx.doi.org/10.1093/oso/9780198719878.003.0014.
Full textF, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textF, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textF, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textNASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textNASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textNASA low-speed axial compressor for fundamental research. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textF, Weaver Harold, Senyitko Richard G, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. NASA low-speed axial compressor for fundamental research. [Washington, DC]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textUnited States. National Aeronautics and Space Administration. and United States. Army Aviation Systems Command., eds. Unsteady flows in a single-stage transonic axial-flow fan stator row. [Washington, D.C.]: National Aeronautics and Space Administration, 1986.
Find full text1939-, Okiishi T. H., and United States. National Aeronautics and Space Administration., eds. Effects of shrouded stator cavity flows on multistage axial compressor aerodynamic performance. [Washington, DC]: National Aeronautics and Space Administration, 1996.
Find full textYa, Timofeev I., Shipilov S. D, and United States. National Aeronautics and Space Administration., eds. Calculation of the distributed loads on the blades of individual multiblade propellers in axial flow using linear and nonlinear lifting surface theories. Washington, DC: National Aeronautics and Space Administration, 1988.
Find full textD, Montgomery Matthew, Kousen Kenneth A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
Find full textD, Montgomery Matthew, Kousen Kenneth A, and United States. National Aeronautics and Space Administration. Scientific and Technical Information Program., eds. Development of a linearized unsteady Euler analysis for turbomachinery blade rows. [Washington, D.C.]: National Aeronautics and Space Administration, Office of Management, Scientific and Technical Information Program, 1995.
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