Within a narrow band of flight conditions in the transonic regime, interactions between shock-
waves and intermittently separated shear layers result in large amplitude, self-sustained …

Within the transonic regime, the aeroelastic problems exhibit many unique characteristics
compared with subsonic and supersonic cases. Although a lot of research has been carried …

Page 1 E. Garnier N. Adams P. Sagaut SCIENTIFIC COMPUTATION Large Eddy Simulation
for Compressible Flows Springer Page 2 Large Eddy Simulation for Compressible Flows Page …

In the age of globalization, commercial aviation plays a central role in maintaining our
international connectivity by providing fast air transport services for passengers and freight …

The present study investigates the accurate inference of Reynolds-averaged Navier–Stokes
solutions for the two-dimensional compressible flow over aerofoils with a deep neural …

Abstract An efficient generalized Zonal Detached Eddy Simulation method (ZDES) is
presented, which aims at performing hybrid Reynolds Averaged Numerical Simulation …

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

IN TRANSONIC flow conditions, shock wave/turbulent boundary-layer interaction with
separation may induce largescale instabilities involving the whole flowfield and is known as …

A transonic flow over the OAT15A supercritical profile is considered. The interaction
between the shock wave and the turbulent boundary layer is investigated through numerical …

A robust strategy for the RANS shielding of attached boundary layers in a hybrid RANS/LES
context is presented, addressing two major issues. Firstly, the attached boundary layers …