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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

Jim A. Penland, James B. Hallissy, and James L. Dillon
Format
EBook; Book; Government Document; Online
Published
Washington, District of Columbia : National Aeronautics and Space Administration, Scientific and Technical Information Branch, December 1979.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1552
Description
1 online resource (144 pages) : illustrations.
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).
Series Statement
NASA technical paper ; 1552
NASA technical paper 1552
Copyright Not EvaluatedCopyright Not Evaluated
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Title from title screen (viewed Sept. 22, 2014).
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