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

Bibliographic Details

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.
Subjects:	Mach number. Pressure measurement. Reynolds number. Transonic wind tunnels. Wind tunnel calibration.
Online Access:	https://purl.fdlp.gov/GPO/gpo71172