An edition of A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel (1980)

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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A fan pressure ratio correlation in terms of ...
Pierce L Lawing
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Last edited by Open Library Bot
December 3, 2010 | History
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An edition of A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel (1980)

A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel

by

  • 0 Ratings
  • 0 Want to read
  • 0 Currently reading
  • 0 Have read

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Publish Date
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
Language
English
Pages
18

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Subjects
Aerodynamics, Transonic, Ground simulators, Low temperature engineering, Testing, Transonic Aerodynamics, Wind tunnels

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Cover of: A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
A fan pressure ratio correlation in terms of Mach number and Reynolds number for the Langley 0.3-meter transonic cryogenic tunnel
1980, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
in English
  • Not in Library

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Book Details

Edition Notes

"Langley Research Center."

Nov. 1980

Includes bibliograpahical references

Published in
Washington, D.C, [Springfield, Va
Series
NASA technical paper -- 1752

The Physical Object

Pagination
18 p. :
Number of pages
18

ID Numbers

Open Library
OL14932774M

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December 3, 2010 Edited by Open Library Bot Added subjects from MARC records.
January 20, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page