Performance of single-stage axial-flow transonic compressor with rotor and stator aspect ratios of 1.63 and 1.78, respectively, and with design pressure ratio of 1.82 / Royce D. Moore and Lonnie Reid.

Bibliographic Details
Uniform Title:NASA technical paper ; 1974.
Main Author: Moore, Royce D.
Corporate Authors: Lewis Research Center
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Other Authors: Reid, Lonnie
Language:English
Published: Washington, D.C. : [Springfield, Va.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch ; [For sale by the National Technical Information Service], 1982.
Series:NASA technical paper ; 1974.
Subjects:
Physical Description:111 pages : illustrations ; 28 cm.
Format: Government Document Book

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