An edition of 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)

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

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Aerodynamic characteristics of a hypersonic r ...
Jim A. Penland
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Last edited by MARC Bot
December 9, 2022 | History
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An edition of 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)

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

by

  • 0 Ratings
  • 0 Want to read
  • 0 Currently reading
  • 0 Have read

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Publish Date
Publisher
National Aeronautics and Space Administration, Scientific and Technical Information Branch
Language
English
Pages
144

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Subjects
Aerodynamics, Aerodynamic characteristics, Computational fluid dynamics, Delta wings, Hypersonic aircraft, Wind tunnel tests

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Cover of: 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
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

Published in
Washington, D.C
Series
NASA technical paper -- 1552, NASA technical paper -- 1552.

The Physical Object

Pagination
1 online resource (144 pages)
Number of pages
144

ID Numbers

Open Library
OL43506463M
OCLC/WorldCat
761863635

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