Item Details

Pressure Distributions on Blunt-Delta Wings at Angles of Attack Up to 90 Degrees and Mach Number of 6.85

by Peter T. Bernot
Format
Book; Government Document; Online; EBook
Published
Washington, D.C. : National Aeronautics and Space Administration : [For sale by the Office of Technical Services, Dept. of Commerce], [1963]
Language
English
Series
NASA Technical Note
SuDoc Number
NAS 1.14:D-1954
Description
39 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • Cover title.
  • "July 1963."
  • Includes bibliographical references.
Series Statement
NASA technical note ; NASA TN D-1954
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Pressure distributions on blunt-delta wings at angles of attack up to 90 degrees and Mach number of 6.85 / c| by Peter T. Bernot.
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    a| Mach number.
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    a| Wings (Anatomy)
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