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NASA Technical Note [NASA TN D-4909]: Effects of angle of attack and bluntness on the shock-layer properties of a 15 degree cone at a mach number of 10.6

By: Contributor(s): Material type: TextTextLanguage: English Series: National Aeronautics and Space Administration | NASA Technical NotePublication details: NASA 1968 WashingtonDescription: 38pSubject(s):
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Bound together NASA TN D-4900 to 4910

Bound vol. Acc. No. 101121 contains Acc. No. TR13259 to TR13268

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