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 present investigation is aimed towards the effect of passive methods on the
performance of supersonic air intake along with the control of shock wave boundary layer …

Computational study of flow physics inside the mixed compression air intake has been
carried out with and without air jets (AJs) at design Mach number of 2.2. Reynolds-averaged …

A numerical study on the performance parameters of supersonic mixed compression air
intake has been carried out at a design Mach number of 2.2 with and without air jets at …

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 …

For the problem that when wheat is sucked up by the air suction method, the seeds are
gathered in a small area, making it difficult for the contact seed cleaning mechanism to clean …

The aim of this work is to increase the C Lmax of NACA 23024 conventional airfoil using the
active flow control mechanism known as the co-flow jet approach. The upper section of the …

The major problem with the Scramjet engine is the starting and unstarting conditions, which
depend on intake performance. Although the engine starts efficiently at designed conditions …

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 …