An edition of Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (1985)

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

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Pressure distributions from high Reynolds num ...
William G. Johnson, William G. ...
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Last edited by Open Library Bot
December 3, 2010 | History
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An edition of Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel (1985)

Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel

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Publish Date
Publisher
NASA
Pages
266

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Subjects

Airfoils
Edition Availability
Cover of: Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
Pressure distributions from high Reynolds number tests of a Boeing BAC I airfoil in the Langley 0.3-Meter Transonic Cryogenic Tunnel
1985, NASA

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Book Details

Edition Notes

Published in
Washington

The Physical Object

Pagination
266 p. :
Number of pages
266

Edition Identifiers

Open Library
OL19985529M

Work Identifiers

Work ID
OL8298071W

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Download catalog record: RDF / JSON
December 3, 2010 Edited by Open Library Bot Added subjects from MARC records.
December 10, 2009 Created by WorkBot add works page