Numerical method for design of minimum-drag supersonic wing camber with constraints on pitching moment and surface deformation /

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Bibliographic Details
Main Authors: Sorrells, Russell B. (Author), Miller, David S. (Author)
Corporate Author: Langley Research Center
Format: Government Document Electronic eBook
Language:English
Published: Washington, D.C. : National Aeronautics and Space Administration, December 1972.
Series:NASA technical note ; D-7097.
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Online Access:CONNECT