Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction
Numerical Study on Wall Temperature Effects on Shock Wave/Turbulent Boundary-Layer Interaction
The effect of wall temperature on the size of the separation bubble in the shock wave/turbulent boundary-layer interaction of a 24 deg compression ramp with Mach 2.9 is numerically investigated. The ratios of wall temperature to recovery temperature are 0.6, 1.14, 1.4, and 2.0, respectively. To validate the simulation, the …