Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds

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Wind tunnel pressure study and Euler code val ...
Patsy S. Fulton.
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Last edited by WorkBot
January 20, 2010 | History

Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds

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Cover of: Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
Wind tunnel pressure study and Euler code validation of a missile configuration with 77 ̊swept delta wings at supersonic speeds
1988, National Aeronautics and Space Administration, Langley Research Center, National Technical Information Service, distributor
Microform in English

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Book Details


Edition Notes

Cover title.

Distributed to depository libraries in microfiche.

"November 1988."

Includes bibliographical references (p. 23).

Microfiche. [Washington, D.C.? : National Aeronautics and Space Administration, 1988] 2 microfiches : negative.

Published in
Hampton, Va, [Springfield, Va
Series
NASA technical memorandum -- 101531.

The Physical Object

Format
Microform
Pagination
vi, 115 p.
Number of pages
115

ID Numbers

Open Library
OL15407176M

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