An edition of Application of shock tubes to transonic airfoil testing at high Reynolds number (1978)

Application of shock tubes to transonic airfoil testing at high Reynolds number

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Application of shock tubes to transonic airfo ...
United States. National Aerona ...
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Last edited by WorkBot
January 20, 2010 | History
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An edition of Application of shock tubes to transonic airfoil testing at high Reynolds number (1978)

Application of shock tubes to transonic airfoil testing at high Reynolds number

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Publish Date
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Technical Information Service
Language
English
Pages
63

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Subjects

Shock tubes, Aerofoils
Edition Availability
Cover of: Application of shock tubes to transonic airfoil testing at high Reynolds number
Application of shock tubes to transonic airfoil testing at high Reynolds number
1978, National Aeronautics and Space Administration, Scientific and Technical Information Office, for sale by the National Technical Information Service
in English
  • Not in Library

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Book Details

Edition Notes

Nov. 1978

Includes bibliographical references

Published in
[Washington], Springfield, Va
Series
NASA technical paper ; 1268

The Physical Object

Pagination
vi, 63 p. :
Number of pages
63

ID Numbers

Open Library
OL14932126M

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January 20, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page