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 …

We present a general strategy to unify wall-resolved and wall-modeled large-eddy
simulation (LES) approaches for turbulent wall-bounded compressible flows. The proposed …

Three-dimensional high-fidelity numerical simulations of a Mach 5 hypersonic ramjet intake
are performed combining a high-order and time-accurate large-eddy-simulation model with …

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

The work describes a systematic optimization strategy for designing hypersonic inlet intakes.
A Reynolds-averaged Navier-Stokes database is mined using genetic algorithms to develop …

This study discusses a general framework to identify the unsteady features of a flow past an
oscillating aerofoil in deep dynamic stall conditions. In particular, the work aims at …

A new idea of nosebleed air jets with strong coupled internal and external flow is put forward
using the lateral jet control principle to improve the maneuverability and fast reaction …

View Video Presentation: https://doi. org/10.2514/6.2022-0181. vid We present our
methodology concerning wall-bounded flow modelling: A unifying strategy for wall-modelled …

The present paper focuses on the Lagrange optimization of shock waves for a two-
dimensional hypersonic inlet by limiting the cowl internal angle and inlet length. The results …

View Video Presentation: https://doi. org/10.2514/6.2021-4199. vid The present study
proposes a robust optimisation strategy for the automatic shaping of inlet intakes in strong …