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Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows

Effects of nose bluntness and shock-shock interactions on blunt bodies in viscous hypersonic flows

D. J. Singh

Details

OL Work ID
OL11671621W

Subjects

Aerodynamics, HypersonicBlunt leading edgesFlow distributionForebodiesHypersonic AerodynamicsHypersonic flowNational Aerospace Plane ProgramNavier-Stokes equationsNoses (forebodies)Viscous flow

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