Computation of nonequilibrium three-dimensional inviscid flow over blunt-nosed bodies flying at supersonic speeds
8th Fluid and PlasmaDynamics Conference ; 1975 ; Hartford , CT , U.S.A.
1975-01-01
Conference paper
Electronic Resource
English
Flow separation ahead blunt bodies at supersonic speeds
TIBKAT | 1951
|THREE-DIMENSIONAL APPROXIMATE VISCOUS SHOCK LAYER METHOD FOR HYPERSONIC FLOW OVER BLUNT-NOSED BODIES
British Library Conference Proceedings | 2003
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