The interaction between an incident shock wave and a Mach-6 undisturbed hypersonic
laminar boundary layer over a cold wall is addressed using direct numerical simulations …

The current study discusses how numerical schemes and discretization approaches affect
wall-resolved and wall-modeled LES outcomes. A turbulent boundary layer setup over a flat …

The excessive computational resource requirements for direct numerical simulation (DNS)
and wall-resolved large eddy simulation (LES) make these methods intractable for …

The present paper discusses the physical reliability of turbulence modeling in an adverse
pressure gradient wall flow setup at moderate/high Reynolds number by comparing wall …

View Video Presentation: https://doi. org/10.2514/6.2021-1438. vid We perform wall-
modeled large eddy simulations (WMLES) of turbulent flow over a Gaussian-shaped bump …

View Video Presentation: https://doi. org/10.2514/6.2022-0676. vid Interaction between
physical systems in nature occur seamlessly, where two or more processes affect each other …

The current work presents an innovative numerical technique for high-Reynolds/high-Mach
number compressible flow simulations in complex configurations. In particular, the research …

Accurate prediction of aerothermal surface loading is of paramount importance for the
design of high-speed flight vehicles. In this work, we consider the numerical solution of …

View Video Presentation: https://doi. org/10.2514/6.2022-4006. vid The majority of
atmospheric entry vehicles use heat shields made of thermal protection materials that ablate …

The use of wall-modeled large-eddy simulation (WMLES) is explored in the context of
compressible flows with a focus on cold-wall boundary layers and flows with shock-induced …