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 …

Stereoscopic particle image velocimetry is used to investigate the effects of micro-ramp sub-
boundary layer vortex generators, on an incident shock wave/boundary layer interaction at …

The shock wave/turbulent boundary layer interaction (SWBLI) exists widely in the internal
and external supersonic flow field. The interaction of shock waves with turbulent boundary …

Flow control can be applied to shock wave/boundary layer interactions to achieve two
different goals; the delay of shock-induced separation and/or the reduction of stagnation …

OBLIQUE shock boundary-layer interactions (SBLIs) occurring in mixed compression engine
inlets have been a cause of concern to the aerospace industry. Shock-induced separation of …

A direct numerical simulation study is performed on the hypersonic shock wave/boundary
layer interaction controlled by using a microramp vortex generator (MVG). The mean …

Various types of micro-vortex generators (μVGs) are investigated for control of a supersonic
turbulent boundary layer subject to an oblique shock impingement, which causes flow …

An implicit large eddy simulation, implemented using a fifth-order, bandwidth-optimized
weighted essentially non-oscillatory scheme, was used to study the flow past a compression …

ICRO vortex generator (VG) is a kind of low-profile passive control devices designed for the
boundary layer control. Contrasting to the conventional vortex generator which is widely …

Supersonic intakes must provide a stable, uniform, low-loss, subsonic flow to the engine
face at all flight conditions. Shock losses place an upper limit on the flight Mach number of …