Murthy, AV (1974) Hypersonic flow over blunted slender wedges. Journal of Aircraft, 11 . pp. 649-651. ISSN 0021-8669Full text not available from this repository.
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:||Journal 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 09:55|
Actions (login required)