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三维直角叉树切割网格Euler方程自适应算法 被引量:7

A 3D adaptive algorithm of Cartesian grid for Euler equations
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摘要 基于叉树数据结构,实现了一种用于三维直角叉树切割网格的自适应算法,包括对几何外形,以及对流场计算的自适应网格加密技术。在初始网格的生成过程中,根据相邻网格的物面法向向量间的差值,进行针对外形的自适应网格加密;在流场计算中,根据相邻网格间选定物理量梯度的变化,进行针对流场的自适应网格加密。详细地描述了三维直角叉树切割网格的生成过程,以及对任意网格的切割细分算法。在自适应过程中,分别采用了八叉树和全叉树的数据结构,八叉树是基本的数据结构,而全叉树的采用,使网格具有了各向异性的特征,从而大大的减少了自适应网格的数量。采用中心有限体积法,求解Euler方程,并运用上述方法,完成了对外形和流场的自适应网格加密算法,获得了较好的数值计算结果,证明了自适应算法的正确性,体现了直角叉树切割网格自适应技术的有效性和实用性。 The paper presents an adaptive refinement method of the Cartesina grid for the Euler equations.Given the definition of body configuration,geometrybased refinement of Cartesian grids is generated automatically through cellcutting algorithm.Solutionbased grid adaptations are carried out after converged solutions are obtained on a given grid.In the course of initial grid generation,a twostep raycasting algorithm to excluded cells inside the body and a cellmerging technique to avoid numerical insability are described.An Octree and Omnitree data structure has beed to store the data,which respectively support isotropic and anisotropic grid refinement.For the sake of flow calculation,four separate data entities are defined.A flow solver of the Euler equations is performed by a conventional algorithms,including finite volume method and RungeKutta tinestepping scheme.The flow solver supports arbitrary control volume.Based on the above approach,the numerical analysis of flows around ONERA M6 wing and the wing/body configuration is finished.The numerical results presented show flexibility and accuracy of this approach.
出处 《空气动力学学报》 CSCD 北大核心 2002年第4期394-402,共9页 Acta Aerodynamica Sinica
基金 航空基金资助项目(98A53005) 西北工业大学博士论文创新基金资助项目
关键词 直角叉树切割网格 自适应算法 叉树数据结构 EULER方程 计算流体力学 Cartesian grid adaptation technique tree data structure
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参考文献6

  • 1WANG Z J.Proof of concept-an automatic CFD computing environment with a cartesian prism grid generator,grid adaptor and flow solver[C].in Proceeding of 4th International Meshing Roundtable,October 1995 87-99,Albuquerque,New Mexico.
  • 2JOHN E M,MARSHA J B,MICHAEL j A,MICHAEL D.W.3D application of a Cartesian grid Euler method[R].AIAA 95-0853,1995.
  • 3KARMAN S l.SPLITFLOW:A 3D unstructured Cartesian/prismatic grid CFD code for complex grometries[R].AIAA-95-0343,1995.
  • 4STOLCIS L.JOHNSTON L J.Solution of the Euler equation on unstructrued grids for two-dimensional compressible flow[J].Aeronautical Journal 1990 June/July.
  • 5SWANSON R C.TURKEL E.Artificial dissipation and central difference schemes for the Euler and Navier-Stokes equtions[R].AIAA Paper,87-1107,1987.
  • 6DARREN D Z.KENNETH G P.An adaptively-refined cartesian mesh slover fhr the euler Equation[R].AIAA-95-0343,1995.

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