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 research on shock wave/turbulent boundary-layer interactions is mainly limited to
calorically perfect gases; little has been reported on the thermochemical non-equilibrium …

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 …

Shock wave/turbulent boundary layer interactions are widely observed in supersonic flows
with many adverse effects on the flow field, resulting in increasing investigation on their …

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 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 …

Shock wave/boundary layer interaction (SWBLI) is a common phenomenon occurring in the
supersonic/hypersonic flow fields, and it can constrain the performance of the vehicle. In the …

Magnetohydrodynamic (MHD) heat shield systems have been proven to be highly effective
in hypersonic blunt-nosed bodies. Thus, it is natural to consider the application of MHD to …

Air-blowing is one of the techniques for active flow control and thermal protection system of
hypersonic vehicles. Introducing air into the hypersonic boundary layer alters the cross …