Cover Image

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
Description
Item Description:Title from title screen (viewed on Aug. 17, 2016).
"November 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Physical Description:1 online resource (18 pages) : illustrations.
Bibliography:Includes bibliographical references (page 11).