Recent advances in shock wave boundary layer interaction research are reviewed in four
areas:(i) understanding low frequency unsteadiness,(ii) heat transfer prediction …

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 …

With the maturation of the scramjet technologies, the urgent development of the combined
cycle propulsion system has been put forward, and it can help the vehicle to launch and land …

THE aerodynamic design of inlets for supersonic flight has commonly included the use of
porous bleed regions to reduce the adverse effects of shock wave/boundary-layer …

To investigate whether vortex generators can be an effective form of passive flow control an
experimental investigation has been conducted in a small-scale wind tunnel. With specific …

Various flow control devices have been conceived for hypersonic inlets to suppress the inlet
unstart and reduce the total pressure loss over the wide range of operating conditions of …

Compressible particle-resolved direct numerical simulations (PR-DNS) are widely used in
explosion-driven dispersion of particles simulations, multiphase turbulence modelling, and …

This work presents results from large-eddy/Reynolds-averaged Navier–Stokes (LES/RANS)
simulations of the well-known Burrows–Kurkov supersonic reacting wall-jet experiment …

In this study, we conducted experimental and numerical investigations to assess the effects
of backpressure and configurations of porous bleeds on a scramjet inlet's performance at …

In the experiment reported in this paper, a spanwise array of herringbone riblets strips is
applied upstream of the interaction region between an im**ing shockwave and a turbulent …