Supersonic Flow Past a Family of Blunt Axisymmetric Bodies

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U.S. Government Printing Office, 1959 - Aerodynamics, Supersonic - 25 pages
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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.

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