Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

Comparison of wind tunnel and flight test aft ...
Jack Nugent
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Last edited by Open Library Bot
December 3, 2010 | History

Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

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Cover of: Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds
1988, National Aeronautics and Space Administration, Scientific and Technical Information Branch, For sale by the National Technical Information Service]
Microform in English
Cover of: Comparison of wind tunnel and flight test afterbody and nozzle pressures for a twin-jet fighter aircraft at transonic speeds

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Book Details


Edition Notes

Distributed to depository libraries in microfiche.

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration], 1988. 1 microfiche.

Published in
[Washington, DC], [Springfield, Va
Series
NASA technical paper -- 2588.

The Physical Object

Format
Microform
Pagination
1 v.

Edition Identifiers

Open Library
OL14662959M

Work Identifiers

Work ID
OL11148852W

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History

Download catalog record: RDF / JSON
December 3, 2010 Edited by Open Library Bot Added subjects from MARC records.
January 19, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page