Boundary layer separation is a common phenomenon in supersonic/hypersonic vehicles,
and can adversely affect the lift coefficient. Currently, active flow control based on microjets …

Shock wave/boundary layer interaction (SBLWI) is a common coupling phenomenon that
occurs in hypersonic vehicles, and it adversely affects the flow fields inside and outside the …

The unstable movement of the shock train in a hypersonic inlet–isolator always brings
difficulty to its closed-loop control, and some methods should be taken to stabilize the shock …

激波/边界层干扰现象在超声速流场中不可避免, 这种现象的存在会对超声速飞行器内外流场
产生一系列的不利影响. 所以, 对激波/边界层干扰现象进行控制是十分必要的 …

Shock Wave Boundary Layer Interaction Control has been an active area of research for the
past decades. The effect of SWBLI on the flow filed and on the performance of Supersonic …

This study investigates the performance enhancement of mixed compression supersonic air
intakes through the combined application of bump and bleed techniques. Supersonic air …