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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.

Record details

  • Physical Description: 1 online resource (18 pages) : illustrations.
  • Publisher: [Washington, D.C.] : National Aeronautics and Space Administration, Scientific and Technical Information Branch, November 1980.

Content descriptions

General Note:
Title from title screen (viewed on Aug. 17, 2016).
"November 1980."
"Performing Organization: NASA Langley Research Center"--Report documentation page.
Bibliography, etc. Note:
Includes bibliographical references (page 11).
Type of Report and Period Covered Note:
Technical paper.
Funding Information Note:
National Aeronautics and Space Administration 505-31-53-01

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