Advances in measuring and understanding separated, nominally two-dimensional (2D)
shock-wave/turbulent-boundary-layer interactions (STBLI) have triggered recent campaigns …

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 …

In high-speed flow past a normal shock, the fluid temperature rises rapidly triggering
downstream chemical dissociation reactions. The chemical changes lead to appreciable …

The current generation of axial turbomachines is the culmination of decades of experience,
and detailed understanding of the underlying flow physics has been a key factor for …

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 use of nonlinear, dynamic methods for the simulation of aerospace structures has
increased dramatically in recent years [1]; however, very little relevant experimental data …

We analyse the low-frequency dynamics of a high Reynolds number impinging shock-
wave/turbulent boundary-layer interaction (SWBLI) with strong mean-flow separation. The …

The fluid–structure interaction of a flexible panel exposed to a ramp-induced shock-
wave/boundary-layer interaction (SWBLI) at Mach 6 is investigated experimentally for …

The low-frequency unsteadiness in the direct numerical simulation of a Mach 2.9 shock
wave/turbulent boundary layer interaction with mean flow separation is analysed using …

An experimental methodology was designed to study the effects of turbulent flow and
shock/boundary-layer interaction (SBLI) on the postflutter response of a thin, buckled panel …