A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel / Pierce L. Lawing, Jerry B. Adcock, and Charles L. Ladson.

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Main Authors: Lawing, Pierce L. (Author), Adcock, Jerry B. (Author), Ladson, Charles L. (Author)
Corporate Author: Langley Research Center
Format: Government Document eBook
Language:English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
Series:NASA technical paper ; 1752.
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Call Number: NAS 1.60:1752
NAS 1.60:1752 Available