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NASA TR R-163

Title:NASA TR R-163
Alternate title:Hypersonic shock-heated flow parameters for velocities to 46,000 feet per second and altitudes to 323,000 feet
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Author:
Author:
Note:National Aeronautics and Space Administration ; [For sale by the Office of Technical Services, Department of Commerce, Washington, D.C. 20230], 1963
  
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Subject:Aerodynamics, Hypersonic
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