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Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a Mach number of 2.01 / by Gerald V. Foster.

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Format:
Book
Government document
Author/Creator:
Foster, Gerald V., author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Series:
NASA technical memorandum ; X-134.
NASA/TM ; X-134
Language:
English
Subjects (All):
Aerodynamics, Supersonic.
Supersonic wind tunnels.
Physical Description:
1 online resource (24 pages) : illustrations.
Place of Publication:
[Washington, D.C.] : National Aeronautics and Space Administration, [November 1959].
Notes:
Includes bibliographical references (page 6).
Description based on online resource; title from PDF caption (NASA, viewed on May 26, 2022).
Other Format:
Print version: Foster, Gerald V. Sideslip characteristics at various angles of attack for several hypersonic missile configurations with canard controls at a mach number of 2.01.
OCLC:
761129791

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