Hypersonic flow over blunted slender wedges

Murthy, AV (1974) Hypersonic flow over blunted slender wedges. Journal of Aircraft, 11. pp. 649-651. ISSN 0021-8669

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An attempt is made to show that the results of Stollery et al. (1971) can be obtained in closed form for the pressure and shock wave shape by integrating the equations analytically, as described by the author (1972). Further, it is indicated that the estimates of the method near the leading edge can be improved by incorporating modifications suggested by Kemp (1969) to account for the effect of gamma (ratio of specific heats).

Item Type: Article
Uncontrolled Keywords: Blunt bodies;Hypersonic flow;Inviscid flow;Slender bodies;Wedge flow;Entropy;Flow equations;Pressure distribution;Specific heat
Subjects: AERONAUTICS > Aircraft Design, Testing & Performance
AERONAUTICS > Aerodynamics
Depositing User: Mrs Neetu Chandra
Date Deposited: 07 Dec 2007
Last Modified: 24 May 2010 04:25
URI: http://nal-ir.nal.res.in/id/eprint/4479

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