A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-Meter Transonic Cryogenic Tunnel

Main Author: Lawing, Pierce L.,
Other Authors: Adcock, Jerry B.,, Ladson, Charles L.,, Langley Research Center., United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch,
Format: eBook
Language: English
Published: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
Physical Description: 1 online resource (18 pages) : illustrations.
Series: NASA technical paper ; 1752.
Online Access: https://purl.fdlp.gov/GPO/gpo71172
https://purl.fdlp.gov/GPO/gpo71172

CMU Gov Pub Electronic

LocationCall Number: Status
CMU Gov Pub Electronic NAS 1.60:1752 Online