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Publish Date
1979
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Language
English
Pages
144
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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
1979, National Aeronautics and Space Administration, Scientific and Technical Information Branch
in English
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Book Details
Edition Notes
Title from title screen (viewed Sept. 22, 2014).
"December 1979."
"Performing organization, NASA Langley Research Center"--Technical report documentation page.
Includes bibliographical references (pages 20-22).
Sponsored by National Aeronautics and Space Administration 505-11-33-01
L-13158
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