The shock wave/boundary-layer interaction is a common phenomenon, and it occurs in the
internal and external flow fields of the hypersonic vehicle. Then, the separation, the …

A shock wave/boundary layer interaction is a common phenomenon in supersonic
(hypersonic) flows, and it usually occurs in an airbreathing propulsion system. It induces a …

For a long time, people hold an idea that vorticity is equivalent to vortex for fluid flow since
vorticity represents rotation for rigid body. Nevertheless, many experimental results do not …

The separation bubble caused by the shock wave/boundary layer interaction (SWBLI) has
adverse influence on the field performance, and the passive control approach should be …

The interaction between the shock wave and the turbulence boundary layer induces a
separation, and this is an undesired phenomenon for the flow field performance. The control …

Motivated by the favorable effects of asymmetrical vortical structures on shock-wave
boundary layer interactions, we performed implicit large-eddy simulations to analyze the …

This work demonstrates the control of the shock-induced separated flow generated by a
sharp fin placed on a cylindrical surface (fin-on-cylinder shock-wave/boundary-layer …

We analyze the influence of microramp vortex generators (mVGs) on a canonical oblique
shock wave/turbulent boundary-layer interaction (SBLI) in terms of mean flow field and …

This paper describes the modifications instigated in a flare induced shock–boundary layer
interaction flowfield by two vortex generators viz. Baseline Ramps (BRs) and Ramped …

Vortex structures, detected by the existing popular vortex identification methods, of the same
case are generally different if the results are measured by different observers, who are …