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
Details
- OL Work ID
- OL11671621W
Subjects
Aerodynamics, HypersonicBlunt leading edgesFlow distributionForebodiesHypersonic AerodynamicsHypersonic flowNational Aerospace Plane ProgramNavier-Stokes equationsNoses (forebodies)Viscous flow