Transonic wind-tunnel tests of an F-8 airplane model equipped with 12- and 14- percent thick oblique wings

Transonic wind-tunnel tests of an F-8 airplan...
Ronald C. Smith, Ronald C. Smi...
Transonic wind-tunnel tests of an F-8 airplane model equipped with 12- and 14- percent thick oblique wings by Ronald C. Smith, Ronald C. Smith
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Transonic wind-tunnel tests of an F-8 airplane model equipped with 12- and 14- percent thick oblique wings

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Publish Date
Language
English

Book Details


Edition Notes

Published in
Moffett Field, California
Series
Technical memoranda / National Aeronautics and Space Administration -- TM-X-62478

Edition Identifiers

Open Library
OL13840975M

Work Identifiers

Work ID
OL4305495W

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