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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

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@ University of Illinois

Lawing, Pierce L

Description

Nov. 1980."Langley Research Center."Includes bibliographical references.
Type:
Text
Format:
Language Material Electronic Resource
Contributors:
Ladson, Charles LAdcock, Jerry BLangley Research CenterUnited States. National Aeronautics and Space Administration. Scientific and Technical Information Branch
Rights:
Public domain. Learn more at http://www.hathitrust.org/access_use
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Record Contributed By

University of Illinois

Record Harvested From

HathiTrust

Keywords

  1. Aerodynamics, Transonic
  2. Ground Simulators
  3. Low Temperature Engineering
  4. Testing
  5. Wind Tunnels

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