An edition of Effect of fin leading edge sweep on shock-shock interaction at Mach 6 (1996)

Effect of fin leading edge sweep on shock-shock interaction at Mach 6

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Effect of fin leading edge sweep on shock-sho ...
Scott A. Berry
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Last edited by WorkBot
January 21, 2010 | History
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An edition of Effect of fin leading edge sweep on shock-shock interaction at Mach 6 (1996)

Effect of fin leading edge sweep on shock-shock interaction at Mach 6

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Publish Date
Publisher
American Institute of Aeronautics and Astronautics, [National Aeronautics and Space Administration, National Technical Information Service, distributor
Language
English

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Subjects

Reynolds number, Wind tunnel tests, Leading edge sweep, Hypersonic speed, Shock wave interaction

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Cover of: Effect of fin leading edge sweep on shock-shock interaction at Mach 6
Effect of fin leading edge sweep on shock-shock interaction at Mach 6
1996, American Institute of Aeronautics and Astronautics, [National Aeronautics and Space Administration, National Technical Information Service, distributor
Microform in English
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Book Details

Edition Notes

Shipping list no.: 98-0007-M.

Microfiche. [Washington, D.C. : National Aeronautics and Space Administration, 1997] 1 microfiche.

Published in
Washington, DC, Springfield, Va
Series
NASA technical memorandum -- 111790.

The Physical Object

Format
Microform
Pagination
1 v.

ID Numbers

Open Library
OL15501765M

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January 21, 2010 Edited by WorkBot add subjects and covers
December 11, 2009 Created by WorkBot add works page