Item Details

Supersonic Flow Past a Family of Blunt Axisymmetric Bodies

by Milton D. Van Dyke and Helen D. Gordon
Format
Book; Government Document; Online; EBook
Published
Washington, DC : U.S. G.P.O., 1959.
Language
English
Series
NASA. Tr
Summary
Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached bow waves. The gas is assumed perfect with y=5/3, 7/5, or 1. Free-stream Mach numbers are taken as 1.2, 1.5, 2, 3, 4, 6, 10, and [infinity symbol]. The results are summarized with emphasis on the sphere and paraboloid.
Description
25 p. : ill. ; 26 cm.
Mode of access: Internet.
Notes
  • "Report date Oct. 2, 1958."
  • Includes bibliographical references (p. 16).
Series Statement
NASA. TR ; R-1
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| Van Dyke, Milton.
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    a| Supersonic flow past a family of blunt axisymmetric bodies / c| by Milton D. Van Dyke and Helen D. Gordon.
    260
      
      
    a| Washington, DC : b| U.S. G.P.O., c| 1959.
    300
      
      
    a| 25 p. : b| ill. ; c| 26 cm.
    490
    0
      
    a| NASA. TR ; v| R-1
    500
      
      
    a| "Report date Oct. 2, 1958."
    504
      
      
    a| Includes bibliographical references (p. 16).
    520
      
      
    a| Some 100 numerical computations have been carried out for unyawed bodies of revolution with detached bow waves. The gas is assumed perfect with y=5/3, 7/5, or 1. Free-stream Mach numbers are taken as 1.2, 1.5, 2, 3, 4, 6, 10, and [infinity symbol]. The results are summarized with emphasis on the sphere and paraboloid.
    538
      
      
    a| Mode of access: Internet.
    650
      
    0
    a| Shock waves.
    650
      
    0
    a| Aerodynamics, Supersonic.
    700
    1
      
    a| Gordon, Helen D.
    710
    1
      
    a| United States. b| National Aeronautics and Space Administration.
    710
    2
      
    a| Ames Research Center.
    974
      
      
    b| UIU c| UIUC d| 20141113 s| google u| uiug.30112106908426 y| 1959 r| pd q| bib

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