Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading
By: Nelson L. Sanger and Raymond P. Shreeve.
Contributors: Shreeve, Raymond P.; Lewis Research Center.
Series: NASA technical memorandum -- 87167.
Publisher: National Aeronautics and Space Administration, Lewis Research Center
Published: 1986
Place of publication: [Cleveland, Ohio
Language: eng
Format: Microform
Subjects: Compressors -- Blades.; Gas-turbines.; Boundary layers.; Cascade flow.; Comparison.; Compressor blades.; Compressors.; Computation.; Diffusion.; Experimentation.; Gas turbine engines.; Inviscid flow.; Reynolds number.; Stators.; Surface layers.
Notes: Microfiche. [Washington, D.C. : National Aeronautics and Space Administration], 1986. 1 microfiche.