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 hypersonic inlet/isolator acts as the “compressor” for scramjet engines through a series of
shocks, which induces complex internal flows. This paper comprehensively reviews the …

The present paper aims to provide a summary report on recent research progress about
unstart mechanism, detection and control of hypersonic inlet to help the researchers working …

The effect of micro-vortex generators (MVGs) on shock wave/boundary layer interactions
(SBLIs) has been reviewed. Experimental and computational evidence has been presented …

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 …

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 …

This book is elegantly composed for an average student who is interested in learning the
fundamentals of aerodynamics. Even if they do not have any background in aerodynamics …

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 …

This paper experimentally and numerically investigates the effect of shock waves on
transpiration cooling of a porous plate. The experiments were conducted in a wind tunnel of …

We conducted experiments in a wind tunnel with Mach number 2 to explore the evolution of
a transverse plasma jet and its modification effect on a shock wave induced by a ramp with …