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Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers from 0.80 to 1.20, with summary of data from 0.20 to 6.0 /

Bibliographic Details
Main Authors: Penland, Jim A. (Author), Hallissy, James B. (Author), Dillon, James L. (Author)
Corporate Author: Langley Research Center (Author)
Format: Government Document Online Book
Published: Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979.
Series:NASA technical paper ; 1552.
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