Effects of Supersonic Nozzle Geometry on Characteristics of Shock Wave Structure
Effects of Supersonic Nozzle Geometry on Characteristics of Shock Wave Structure
Interaction between the normal shock wave and the turbulent boundary layer in a supersonic nozzle becomes complex with an increase of a Mach number just before the shock wave. When the shock wave is strong enough to separate the boundary layer, the shock wave is bifurcated, and the 2nd and …