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Experimental performance of a 13.65-centimeter-tip-diameter tandem-bladed sweptback centifugal compressor designed for a pressure ratio of 6/

Main Author:	Klassen, Hugh A.
Corporate Authors:	United States National Aeronautics and Space Administration Scientific and Technical Information Office, United States. National Aeronautics and Space Administration. Scientific and Technical Information Office, Lewis Research Center
Other Authors:	Wood, Jerry R.
Format:	Book
Language:	English
Published:	Washington: National Aeronautics and Space Administration, Scientific and Technical Information Office, 1977
Series:	NASA technical paper 1091
Subjects:	Compressors

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