Comparison of calculated and experimental cascade performance for controlled-diffusion compressor stator blading [microform] / Nelson L. Sanger and Raymond P. Shreeve.

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Bibliographic Details
Main Author:	Sanger, Nelson L.
Corporate Author:	Lewis Research Center
Other Authors:	Shreeve, Raymond P.
Format:	Government Document Microfilm Book
Language:	English
Published:	[Cleveland, Ohio] : [National Aeronautics and Space Administration, Lewis Research Center], [1986]
Series:	NASA technical memorandum ; 87167.
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.

Norlin Library - Government Information - Microform

Holdings details from Norlin Library - Government Information - Microform
Call Number:	NAS 1.15:87167
NAS 1.15:87167	Restricted Place a Hold