HYBRID RANS-LES SIMULATION OF WINGTIP VORTEX DYNAMICS

被引:0
|
作者
Kolomenskiy, Dmitry [1 ]
Paoli, Roberto [2 ]
Boussuge, Jean-Francois [2 ]
机构
[1] McGill Univ, Dept Math & Stat, Ctr Rech Math, Montreal, PQ H3H 1Y2, Canada
[2] CERFACS, F-31057 Toulouse 01, France
关键词
LARGE-EDDY SIMULATION; NEAR-FIELD; AEROACOUSTICS; INSTABILITY; TURBULENCE; DIFFUSION;
D O I
暂无
中图分类号
TH [机械、仪表工业];
学科分类号
0802 ;
摘要
This paper presents a feasibility study of a hybrid RANS LES approach to numerical simulation of aircraft wing-tip vortices. A NACA 0012 wing is considered for which earlier published experimental and numerical data are available. Mesh sensitivity tests of our RANS solver and comparisons between two different turbulence models indicate that the RANS approach adequately describes the flow upstream from the trailing edge, but overestimates the rate of decay of the wing-tip vortex. A hybrid RANS LES method is presented that results in a better agreement with the wind tunnel experiment, hence this approach is suggested for numerical simulation of the wake of an airliner.
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页数:11
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