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Author Lawing, Pierce L., author.

Title 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.

Publication Info. [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
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Connect to http://purl.fdlp.gov/GPO/gpo71172

Copies

Location Call No. OPAC Message Status
 Axe Federal Documents Online  NAS 1.60:1752    ---  Available
Description 1 online resource (18 pages) : illustrations.
text txt rdacontent
computer c rdamedia
online resource cr rdacarrier
Series NASA technical paper ; 1752
NASA technical paper ; 1752.
Note Title from title screen (viewed on Aug. 17, 2016).
"November 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography Includes bibliographical references (page 11).
Type Of Report Technical paper.
Funding National Aeronautics and Space Administration 505-31-53-01
L-13713
Subject Aerodynamics, Transonic.
Wind tunnels -- Ground simulators -- Testing.
Low temperature engineering.
Mach number.
Pressure measurement.
Reynolds number.
Transonic wind tunnels.
Wind tunnel calibration.
Genre/Form Online resources.
Electronic books.
Electronic government information.
Added Author Adcock, Jerry B., author.
Ladson, Charles L., author.
Langley Research Center.
United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Other Form: Print version: Lawing, Pierce L. Fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel (OCoLC)7437680
Microfiche version: Lawing, Pierce L. Fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel (OCoLC)711544796
Gpo Item No. 0830-H-15 (online)
Sudoc No. NAS 1.60:1752

 
    
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