Review of computational methods for aerodynamic analysis of iced lifting surfaces

SJ Stebbins, E Loth, AP Broeren… - Progress in Aerospace …, 2019 - Elsevier
Extensive experimental studies and associated reviews have been conducted to better
understand the aerodynamic impact of iced lifting surfaces based on measurements. This …

Towards an enhanced protection of attached boundary layers in hybrid RANS/LES methods

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 …

Modeling in-flight ice accretion under uncertain conditions

G Gori, PM Congedo, O Le Maître, T Bellosta… - Journal of Aircraft, 2022 - arc.aiaa.org
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 …

Zonal detached-eddy simulation applied to the tip-clearance flow in an axial compressor

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 rapid and low noise switch from RANS to WMLES on curvilinear grids with compressible flow solvers

S Deck, PE Weiss, N Renard - Journal of Computational Physics, 2018 - Elsevier
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 …

An improved laminar–turbulent transition cavitation model using the IDDES method

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 …

Advanced numerical prediction of iced airfoil aerodynamics

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 …

Improved prediction of flow around airfoil accreted with horn or ridge ice

M Xiao, Y Zhang - AIAA Journal, 2021 - arc.aiaa.org
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 …

Aerodynamics of a common research model wing with leading-edge ice shape

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 …

Numerical study of iced airfoils with horn features using large-eddy simulation

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 …