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Applications Of A Variational Multiscale Method For Large Eddy Simulation Of Turbulent Flows On Moving/deforming Unstructured Grids

机译:变分多尺度方法在非结构网格移动/变形中湍流大涡模拟中的应用

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In this paper, the three-level formulation of a variational multiscale (VMS) large eddy simulation (LES) method for compressible flow computations [B. Koobus, C. Farhat, A variational multiscale method for the large eddy simulation of compressible turbulent flows on unstructured meshes-application to vortex shedding, Comput. Methods Appl. Mech. Eng. 193 (2004) 1367-1384; C. Farhat, A. Rajasekharan, B. Koobus, A dynamic variational multiscale method for large eddy simulations on unstructured meshes, Comput. Methods Appl. Mech. Eng. 195 (2006) 1667-1691] is extended for applications involving moving/deforming grids. A consistent method to improve the VMS-LES method by computing the small scale Smagorinsky constant (&_s) dynamically [C. Farhat, A. Rajasekharan, B. Koobus, A dynamic variational multiscale method for large eddy simulations on unstructured meshes, Comput. Methods Appl. Mech. Eng. 195 (2006) 1667-1691; A. Rajasekharan, Variationally consistent multiscale formulations and ALE time integrators for large eddy simulation of turbulent flows on dynamic grids, Ph.D. Dissertation, Stanford University, 2008] as the flow develops (dynamic VMS-LES) is also extended for dynamic grid applications. Two applications of VMS-LES for the simulation of separated flow over moving NACA-0012 extruded airfoil is then presented. The first application involves a qualitative simulation exploring the Knoller-Betz effect [K.D. Jones, C.M. Dohring, M.F. Platzer, Experimental and computational investigation of the Knoller-Betz effect, AIAA J. 36(7) (1998) 1240-1246] of the heaving airfoil at high Strouhal number. The second application is that of the pitching airfoil undergoing dynamic stall. The results predicted by the dynamic VMS-LES method are compared to those obtained with other turbulence models and to experimental data and it is found that the dynamic VMS-LES performs better than the other considered static and dynamic LES models.
机译:在本文中,可压缩流计算的变分多尺度(VMS)大涡模拟(LES)方法的三级公式表示[B. Koobus,C.Farhat,一种变分多尺度方法,用于在非结构化网格上对可压缩湍流进行大涡模拟,应用于涡旋脱落计算。方法应用。机甲。 193(2004)1367-1384; C. Farhat,A。Rajasekharan,B。Koobus,一种针对非结构化网格的大型涡模拟的动态变分多尺度方法,计算机。方法应用。机甲。 195(2006)1667-1691]扩展到涉及移动/变形网格的应用。通过动态计算小规模Smagorinsky常数(&_s)来改进VMS-LES方法的一致方法[C. Farhat,A。Rajasekharan,B。Koobus,一种动态变分多尺度方法,用于非结构化网格上的大型涡模拟,计算。方法应用。机甲。 195(2006)1667-1691; A. Rajasekharan,变分一致的多尺度公式和ALE时间积分器,用于动态网格上湍流的大涡模拟,博士。论文,斯坦福大学,2008]随着流程的发展(动态VMS-LES)也扩展到了动态网格应用。然后介绍了VMS-LES在流动的NACA-0012挤压翼型上模拟分离流的两个应用。第一个应用涉及定性模拟,探索Knoller-Betz效应[K.D.琼斯道林,M.F. Platzer,Knoller-Betz效应的实验和计算研究,AIAA J. 36(7)(1998)1240-1246]高Strouhal数的升沉翼型。第二个应用是俯仰翼型的动态失速。将通过动态VMS-LES方法预测的结果与从其他湍流模型获得的结果和实验数据进行了比较,发现动态VMS-LES的性能优于其他考虑的静态和动态LES模型。

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