The control performance of a pulsed nanosecond dielectric barrier discharge (NSDBD)
plasma actuator with varying pulse voltages and locations on a supersonic compression …

HOCK-wave boundary layer interactions (SWBLIs) are frequently encountered on high-
speed vehicles and inlets, transonic wings, and turbine and helicopter blades. At lower …

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 primary focus of the present survey is to categorize the results of various investigations
on the Shock/Boundary-Layer Interactions (SBLIs), their repercussions, and the effective …

The presence of sidewalls exerts three-dimensional (3D) effects on shock wave/turbulent
boundary layer interaction (SBLI), which results in experimental challenges due to the highly …

To study the effects of Mach number, Reynolds number and deflection angle on the conical
separation vortex generated by swept shock wave/turbulent boundary layer interaction, the …

Abstract A RANS (Reynolds-averaged Navier-Stokes simulation) study is performed on an
internal duct at a free-stream Mach number 4.0, to investigate the internal conical shock …

Shock wave-induced boundary layer interactions are unavoidable in high-speed flows. The
strong adverse pressure gradient imposed by the shock on the incoming undisturbed …

The Navier–Stokes equations were solved using a high-fidelity time-implicit numerical
scheme and an implicit large-eddy simulation approach to investigate plasma-based flow …

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 …