S Deck, N Renard - Journal of Computational Physics, 2020 - Elsevier
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 …
In-flight ice accretion under parametric uncertainty is investigated. Three test cases are presented that reproduce experiments carried out at the NASA's Glenn Icing Research …
W Riéra, J Marty, L Castillon, S Deck - AIAA Journal, 2016 - arc.aiaa.org
This paper presents the study of the tip-clearance flow in an axial compressor using several turbulence-modeling approaches: Reynolds-averaged Navier–Stokes, unsteady Reynolds …
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 …
X Feng, Y Liu, B Wang - Ocean Engineering, 2024 - Elsevier
Prediction of the detachment positions of sheet cavitation remains an unsolved problem, being not only dependent on local pressure but also closely related to the boundary layer …
M Costes, F Moens - Aerospace Science and Technology, 2019 - Elsevier
The paper presents a numerical investigation of the flow around a NACA23012 airfoil with two ice shapes, a spanwise ridge and leading edge roughness. RANS and URANS …
DESPITE advances in aircraft icing-protection systems, icing on aircraft lifting surfaces still poses a grave hazard to aircraft operation by decreasing the maximum lift and control …
S Stebbins, E Loth, A Broeren, M Potapczuk… - Journal of Aircraft, 2021 - arc.aiaa.org
Icing on three-dimensional lifting surfaces has been shown to produce highly complex flowfields. However, there is a lack of experimental and computational information in the …
M Xiao, Y Zhang, F Zhou - Journal of Aircraft, 2019 - arc.aiaa.org
Separated flowfields around two iced airfoils with horn features near stall are numerically studied using wall-modeled large-eddy simulation. The iced airfoils are the GLC305 airfoil …