The Fourth AIAA Computational Fluid Dynamics (CFD) High Lift Prediction Workshop and
the Third Geometry and Mesh Generation Workshop were held collaboratively with the …

This study presents a fully automated Cartesian-grid-based compressible flow solver,
named FrontFlow/Violet Hierarchical Cartesian for Aeronautics based on Compressible-flow …

A new immersed boundary Wall-Modelled Large Eddy Simulation (WMLES) formulation is
developed to study high-lift aerodynamics on the NASA High-Lift Common Research Model …

An assessment of a hybrid Reynolds-averaged Navier–Stokes/large-eddy simulation
(HRLES) approach for CL, max prediction is presented for the NASA High-Lift Common …

High-lift operating conditions of aircraft are known to comprise a series of complex physical
features, making the three-dimensional flow difficult to discern and analyse. In such …

This paper presents further improvements to the immersed boundary method introduced in
[1]. The proposed developments take place during the pre-and post-processing stages of the …

The current state-of-the-practice technology for high-lift aerodynamic simulations is to solve
the Reynolds-Averaged Navier-Stokes (RANS) equations on a fixed grid, or a refinement …

View Video Presentation: https://doi. org/10.2514/6.2022-3209. vid Three types of
unstructured CFD mesh families were generated on the NASA High Lift Common Research …

The current state-of-the-practice technology for high-lift aerodynamic simulations is to solve
the Reynolds-averaged Navier–Stokes (RANS) equations on a fixed grid or a refinement …

Aerodynamic simulations were carried out in the study presented in this paper focusing on
the stall performance of the High-Lift Common Research Model obtained from the fourth …