Hybrid RANS/LES Simulations and Aeroacoustic Analysis of Jet Flows using an hp-Adaptive Discontinuous Galerkin Method

被引:7
|
作者
Basile, Francesca [1 ,2 ,3 ]
Chapelier, Jean-Baptiste [1 ]
Laraufie, Romain [2 ]
Frey, Pascal [3 ]
机构
[1] ONERA Univ Paris Saclay, Dept Aeroelastic, Aerodynam Aeroacoust, F-92322 Chatillon, France
[2] Airbus Operat SAS, Flight Phys Capabil, F-31060 Toulouse, France
[3] Sorbonne Univ, Lab Jacques Louis Lions, F-75005 Paris, France
关键词
DETACHED-EDDY SIMULATION; ELEMENT DYNAMIC-MODEL; MESH ADAPTATION; NOISE PREDICTION; FFOWCS WILLIAMS; LES; TURBULENCE;
D O I
10.1007/s10494-022-00376-0
中图分类号
O414.1 [热力学];
学科分类号
摘要
In this paper, an hp-adaptation strategy designed for discontinuous Galerkin methods is extended and applied to hybrid RANS/LES simulations. The 3D hp-adaptive strategy is suited for tetrahedral and hybrid prismatic/tetrahedral meshes, and relies on a metric-based remeshing approach. The metric field and the polynomial map of the adapted meshes are built from an a posteriori error estimator which couples the measure of the energy associated with the highest-order modes and the inter-element jumps of the solution, combined with a smoothness sensor which guides the choice between h- and p-adaptation. The turbulence modeling relies on a Zonal Detached Eddy Simulation approach. The developed hp-adaptation algorithm is assessed in the context of hybrid RANS/LES simulations of the PPRIME nozzle configuration at diameter-based Reynolds number equal to 106, starting the adaptive process from previously RANS-adapted meshes. Far-field acoustic analysis are performed using a Ffowcs Williams-Hawkings method.
引用
收藏
页码:239 / 273
页数:35
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