Item Details

A 1-Foot Hypervelocity Shock Tunnel in Which High-Enthalpy, Real-Gas Air Flows Can Be Generated With Flow Times of About 180 Milliseconds: Bernard E. Cunningham and Samuel Kraus

Cunningham, Bernard E; Kraus, Samuel; United States. National Aeronautics and Space Administration
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], [1962]
Language
English
Series
NASA Technical Note
SuDoc Number
NAS 1.14:D-1428
Description
43 p.: ill. ; 26 cm.
Mode of access: Internet.
Notes
  • Cover title.
  • "October 1962."
  • Aerodynamics, missiles and space vehicles; Fluid mechanics; Research and development facilities.
  • Includes bibliographical references.
Series Statement
NASA technical note ; NASA TN D-1428
Logo for No Copyright - United StatesNo Copyright - United States
Technical Details

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    a| A 1-foot hypervelocity shock tunnel in which high-enthalpy, real-gas air flows can be generated with flow times of about 180 milliseconds / b| Bernard E. Cunningham and Samuel Kraus.
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    a| Washington, D.C. : b| National Aeronautics and Space Administration : b| [For sale by the Office of Technical Services, Dept. of Commerce], c| [1962]
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    a| 43 p.: b| ill. ; c| 26 cm.
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