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Aerodynamic Characteristics of a Hypersonic Research Airplane Concept Having a 70 ̊Swept Double-Delta Wing at Mach Numbers 0.80 to 1.20, With Summary of Data From 0.20 to 6.0

Jim A. Penland, James B. Hallissy
Format
Book; Government Document
Published
Washington, D.C. : National Aeronautics and Space Administration, Scientific and Technical Information Office ; [Springfield, Va. : For sale by the National Technical Information Service], 1979.
Language
English
Series
NASA Technical Paper
SuDoc Number
NAS 1.60:1552
Description
[145] p. : ill. ; 27 cm.
Notes
  • "Langley Research Center."
  • "December 1979"--Cover.
  • Includes bibliographical references.
Series Statement
NASA technical paper 1552
Technical Details
  • Access in Virgo Classic
  • Staff View

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    a| Aerodynamic characteristics of a hypersonic research airplane concept having a 70 ̊swept double-delta wing at Mach numbers 0.80 to 1.20, with summary of data from 0.20 to 6.0 / c| Jim A. Penland, James B. Hallissy.
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