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 …

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 …

In this study, direct numerical simulation of the dispersion and motion of inertial particles in a
spatially developing compressible turbulent boundary layer at a Mach number of 2 is …

In gas-solid flows, the drag force experienced by solid particles plays a significant role in
determining the fluid dynamics of the system. Although several drag models have been …

To investigate the aerodynamic interference challenges for hypersonic vehicles, a new type
of conceptual TSTO model is considered, which consists of a trapezoid wing as the booster …

High-speed air intakes often exhibit intricate flow patterns, with a specific type of flow
instability known as 'buzz', characterized by unsteady shock oscillations at the inlet. This …

The present investigation is aimed towards the effect of passive methods on the
performance of supersonic air intake along with the control of shock wave boundary layer …

Shock-boundary layer interaction (SBLI) at hypersonic inlets can alter the flow pattern and
impose adverse effects on engine operation if not controlled. A two-dimensional surface …

Direct numerical simulations of channel turbulence laden with inertial particles were
performed to investigate the effects of the Mach number on turbophoresis and the …

Small supersonic vehicle concepts used as research platforms to test new aerospace
technologies, such as advanced propulsion systems or large sensor payloads, require major …