Research Catalog

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

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.
Author
Lawing, Pierce L.
Publication
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.

Available Online

https://purl.fdlp.gov/GPO/gpo71172

Details

Additional Authors
  • Adcock, Jerry B.
  • Ladson, Charles L.
  • Langley Research Center.
  • United States. National Aeronautics and Space Administration. Scientific and Technical Information Branch, issuing body.
Description
1 online resource (18 pages) : illustrations.
Series Statement
NASA technical paper ; 1752
Uniform Title
NASA technical paper ; 1752.
Subject
  • Mach number
  • Pressure measurement
  • Reynolds number
  • Transonic wind tunnels
  • Wind tunnel calibration
Note
  • Title from title screen (viewed on Aug. 17, 2016).
  • "November 1980."
  • "Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography (note)
  • Includes bibliographical references (page 11).
Type of Report (note)
  • Technical paper.
Funding (note)
  • National Aeronautics and Space Administration
Call Number
GPO Internet NAS 1.60:1752
OCLC
marcive761455916
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.
Publisher
[Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
Type of Content
text
Type of Medium
computer
Type of Carrier
online resource
Series
NASA technical paper ; 1752
NASA technical paper ; 1752.
Bibliography
Includes bibliographical references (page 11).
Type Of Report
Technical paper.
Funding
National Aeronautics and Space Administration 505-31-53-01
L-13713
Connect to:
https://purl.fdlp.gov/GPO/gpo71172
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
View in Legacy Catalog