A common denominator between conical-symmetry and conical shock interaction is the
spanwise pressure gradient, which perform more non-uniformity and its interaction flow is …

The paper presents highly detailed two-dimensional numerical simulations of hypersonic
nitrogen and air flows around a double wedge, characterized by a complex shock …

Aerodynamic heating is the main challenge for increasing the speed of hypervelocity
vehicles. In this work, three-dimensional numerical simulations have been performed to …

This work presents a detailed analysis of the shock wave/boundary layer interaction in
hypersonic flows around a double-cone. Numerical simulations have been carried out by …

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 …

In the present study, we investigate the evolution of turbulent statistics and coherent
structures in hypersonic turbulent boundary layers at the Mach number of 5 impinged by …

The hypersonic inlet is more prone to deform when simultaneously subjected to
aerodynamic load and harsh aerothermodynamic load. Moreover, the flow field of the …

In the paper, the results of numerical modeling are presented of the 3D turbulent flows in a
channel with backward-facing step, and argon jets injected into the supersonic crossflow …

The efficacy of immersed boundary (IB) methods with adaptive mesh refinement (AMR)
techniques is assessed in the context of atmospheric entry applications, including effects of …

In this paper, the hypersonic shock-shock interaction control using plasma actuator array is
experimentally studied to explore a new surface thermal protection method of hypersonic …