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Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation / by Russell B. Sorrells and David S. Miller.

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Format:
Book
Government document
Author/Creator:
Sorrells, Russell B., author.
Miller, David S., author.
Contributor:
United States. National Aeronautics and Space Administration, issuing body.
Langley Research Center
Series:
NASA technical note ; D-7097.
NASA/TN ; D-7097
Language:
English
Physical Description:
1 online resource (47 pages) : illustrations
Place of Publication:
Washington, D.C. : National Aeronautics and Space Administration, December 1972.
Notes:
"December 1972."
Includes bibliographical references (page 21).
Online resource, PDF version; title from title page (NASA, viewed on July 1, 2021).
Other Format:
Print version: Sorrells, Russell B. Numerical method for design of minimum-drag supersonic wing camber with constraits on pitching moment and surface deformation
OCLC:
890693636

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