Experimental study on the heat flux of transitional shock wave–boundary layer interaction at Mach 6
Yun Jiao, Zhangyu Ma, Longsheng Xue, Chengpeng Wang, Jianqiang Chen, Keming Cheng
Topics & Concepts
Boundary layerMechanicsMach numberHeat fluxTurbulenceShock waveLaminar flowOblique shockMaterials scienceShock (circulatory)PhysicsHeat transferInternal medicineMedicineFluid Dynamics and Turbulent FlowsComputational Fluid Dynamics and AerodynamicsPlasma and Flow Control in Aerodynamics