The paper summarizes recent developments in boundary layer suction for high-speed air
intakes. Bleed has been efficiently used in supersonic and hypersonic intakes for three …

When the flow past a vehicle flying at high velocity becomes supersonic, shock waves form,
caused either by a change in the slope of a surface, a downstream obstacle or a back …

An experimental study was conducted in a transonic channel to control by mechanical vortex
generator devices the strong interaction between a shock wave and a separated turbulent …

The aim of present investigation is to analyze the unsteady oblique shock train and
boundary layer interactions during the self-excited and forced oscillation. The oblique 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 …

Experiments were conducted to study various kinds of shock wave/boundary layer
interaction (SBLI) in an axisymmetric mixed-compression inlet. Further, some of the …

A transonic interaction between a steady shock wave and a turbulent boundary layer in a
Mach 1.4 channel flow is experimentally investigated by means of particle image velocimetry …

SHOCK/BOUNDARY-LAYER interactions (SBLIs) occur in almost all high-speed
aerodynamic applications. Examples include the wings of aircraft traveling at transonic …

An experimental investigation of the response of an oblique shock train to downstream
periodic pressure perturbations was conducted. The oblique shock train is generated in a …

This paper presents an application of the pressure-sensitive paint technique to investigate
two-dimensional unsteady flow in a transonic channel. This work is a contribution to the …