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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.
Connect to full text Available online
View online- Format:
- Book
- Government document
- Author/Creator:
- Lawing, Pierce L., author.
- Adcock, Jerry B., author.
- Ladson, Charles L., author.
- Series:
- NASA technical paper ; 1752.
- NASA technical paper ; 1752
- Language:
- English
- Subjects (All):
- Aerodynamics, Transonic.
- Wind tunnels--Ground simulators--Testing.
- Wind tunnels.
- Low temperature engineering.
- Genre:
- Online resources.
- Physical Description:
- 1 online resource (18 pages) : illustrations
- Place of Publication:
- [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.
- Notes:
- Title from title screen (viewed on August 17, 2016).
- "November 1980."
- "Performing Organization: NASA Langley Research Center"--Report documentation page
- Includes bibliographical references (page 11).
- Other Format:
- 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
- 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
- OCLC:
- 761455916
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