TY - GEN
T1 - Wall-modeled large eddy simulation of laminar and turbulent separated flows
AU - Cadieux, F.
AU - Sadique, J.
AU - Yang, X. I.A.
AU - Mittal, R.
AU - Meneveau, C.
N1 - Publisher Copyright:
© 2016, American Institute of Aeronautics and Astronautics Inc, AIAA. All rights reserved.
PY - 2016
Y1 - 2016
N2 - The capability of the recently proposed integral wall model for large eddy simulation (iWMLES) to capture flow separation, transition, and reattachment is investigated by means of flow over a flat plate with a suction and blowing boundary condition. Wall-resolving LES can accurately recover time-averaged DNS results for a laminar separation bubble, but are limited to moderate Reynolds numbers due to the strong requirement of resolving the boundary layer. Typical equilibrium wall-models do not take pressure gradients into account, and many hybrid RANS-LES either rely on the equilibrium assumption or require very fine mesh spacing in the wall-normal direction. iWMLES addresses these deficiencies through the addition of non-equilibrium terms in an integral version of the momentum equation. iWMLES of a laminar separation bubble flow confirm that the wall-model can capture flow separation, transition, and reattachment at Reδ = 105 on a coarse grid. Good qualitative agreement with a wall-resolved LES of a turbulent separation bubble is obtained using iWMLES on a coarser wall-normal grid. Trends in both mean and RMS velocities as well as the coefficient of pressure are well predicted by the iWMLES.
AB - The capability of the recently proposed integral wall model for large eddy simulation (iWMLES) to capture flow separation, transition, and reattachment is investigated by means of flow over a flat plate with a suction and blowing boundary condition. Wall-resolving LES can accurately recover time-averaged DNS results for a laminar separation bubble, but are limited to moderate Reynolds numbers due to the strong requirement of resolving the boundary layer. Typical equilibrium wall-models do not take pressure gradients into account, and many hybrid RANS-LES either rely on the equilibrium assumption or require very fine mesh spacing in the wall-normal direction. iWMLES addresses these deficiencies through the addition of non-equilibrium terms in an integral version of the momentum equation. iWMLES of a laminar separation bubble flow confirm that the wall-model can capture flow separation, transition, and reattachment at Reδ = 105 on a coarse grid. Good qualitative agreement with a wall-resolved LES of a turbulent separation bubble is obtained using iWMLES on a coarser wall-normal grid. Trends in both mean and RMS velocities as well as the coefficient of pressure are well predicted by the iWMLES.
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M3 - Conference contribution
AN - SCOPUS:84980329006
SN - 9781624104367
T3 - 46th AIAA Fluid Dynamics Conference
BT - 46th AIAA Fluid Dynamics Conference
PB - American Institute of Aeronautics and Astronautics Inc, AIAA
T2 - 46th AIAA Fluid Dynamics Conference, 2016
Y2 - 13 June 2016 through 17 June 2016
ER -