Axisymmetric hypersonic flow with strong viscous interaction /
by John Webster Ellinwood and Harold Mirels.
Description
- Language(s)
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English
- Published
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Los Angeles, California : Space Systems and Ballistic Systems Divisions, Los Angeles Air Force Station, Air Force Systems Command, United States Air Force, 1967.
- Summary
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Stewartson's theory for axisymmetric hypersonic flow of a model gas with strong viscous interaction and strong shock wave is extended to power-law viscosity variation, nonunit Prandtl number, and body shapes other than power laws. For power-law bodies, the generalized theory is obtained in closed form without recourse to numerical integration. In addition, numerical computations are presented for axisymmetric flow over a three-quarter power-law body with strong shock wave and viscous interactions that range from weak to strong. (Author).
- Note
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"July 1967."
- Physical Description
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39 pages :
illustrations ;
28 cm.
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