Abstract Rayleigh–Taylor (RT) and Richtmyer–Meshkov (RM) instabilities are well-known
pathways towards turbulent mixing layers, in many cases characterized by significant mass …

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

We present a computational analysis of the reactive flow in a hypersonic scramjet engine
with focus on effects of uncertainties in the operating conditions. We employ a novel …

The interaction between isotropic turbulence and a normal shock wave is investigated
through a series of direct numerical simulations at different Reynolds numbers and mean …

A two-length scale, second moment turbulence model (Reynolds averaged Navier-Stokes,
RANS) is proposed to capture a wide variety of single-phase flows, spanning from …

A turbulence model is developed to described the self-similar growth of the Rayleigh-Taylor
(RT) and Richtmyer-Meshkov (RM) instabilities. The model describes the dominant eddies in …

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 …

Menter SST k-ω is a Reynolds-averaged Navier–Stokes based two-equation turbulence
model routinely used in industry for predicting aerodynamic flows. It shows excellent …

Supersonic flows exhibit compressible effects and ignoring this influence would lead
deviations in supersonic combustion simulation. In this study, taking the standard k− ε …

THE characteristics of a turbulent boundary layer in a supersonic flow can be drastically
altered by a shock wave. The interaction can lead to high pressure and heat loads, as well …