The paper provides a brief introduction to the near-wall problem of LES and how it can be
solved through modeling of the near-wall turbulence. The distinctions and key differences …

The book aims to provide the reader with an updated general presentation of multiscale/
multiresolution approaches in turbulent flow simulations. All modern approaches (LES …

RESEARCH to develop high-speed airbreathing aerospace propulsion systems was
underway in the late 1950s. A major part of the effort involved the supersonic combustion …

The present work presents a Zonal Detached Eddy Simulation (ZDES) to simulate a spatially
develo** turbulent boundary layer over a smooth flat plate at Re θ= 2900. Results are …

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 …

A turbulent inflow for a rapid and low noise switch from RANS to Wall-Modelled LES on
curvilinear grids with compressible flow solvers is presented. It can be embedded within the …

To overcome the lack of resolved turbulent flow structures generated by the improved
delayed detached eddy simulation (IDDES) model when simulating the shock wave and …

MEAN flow quantities in attached turbulent boundary layers may be predicted by Reynolds-
averaged Navier–Stokes (RANS) simulations, but resolving the most energetic fluctuations …

UNDERSTANDING the flow physics involved with sonic injection into a supersonic crossflow
plays a vital role in the analysis and design of supersonic combustive ramjet (scramjet) …

THE choice of a numerical technique to examine the structure of shock wave/turbulent
boundary-layer interactions in highspeed engine configurations is one dictated by …