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.
01.01.1975
Aufsatz (Konferenz)
Elektronische Ressource
Englisch
THREE-DIMENSIONAL APPROXIMATE VISCOUS SHOCK LAYER METHOD FOR HYPERSONIC FLOW OVER BLUNT-NOSED BODIES
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