Cowl Shock-Boundary Layer Interaction in Three Dimensional Compression Scramjet Inlet
会议名称：《The 4th Across-strait Workshop on Shock Wave/Vortex Interaction》
会议日期：2008年
学科分类：0810[工学-信息与通信工程] 08[工学] 081001[工学-通信与信息系统]
摘 要：The shock-boundary layer interaction and boundary layer separation are frequently encountered phenomena in hypersonic inlet and play a major role in its ***, the flow is more complicate in three-dimensional compression scramjet inlet by there-dimensional shock-shock and shock-boundary layer *** of researches had basically emphasized on the glancing-shock-induced separation and two-dimensional shock separation,which are included in three-dimensional compression ***,the flow in the isolator has not been adequately studied,especially in which the shocks interact with the turbulent boundary layers in a constrained flow.