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二维非结构网格的生成及其EULER方程解
引用本文:王平,朱自强. 二维非结构网格的生成及其EULER方程解[J]. 北京航空航天大学学报, 2000, 26(2): 190-193
作者姓名:王平  朱自强
作者单位:北京航空航天大学飞行器设计与应用力学系
摘    要: 采用推进阵面法生成三角形非结构网格,用多重网格技术求解泊桑方程以取得结构背景网格.提出了一种高效的边界剖分法,并用它来生成初始阵面.另外,还提出了一种新颖的数据结构——数组链接表,用它来存贮网格数据.用有限体积法在非结构网格中求解了二维可压缩Euler方程,给出了单段翼型和多段翼型的算例,并与实验结果进行了比较和分析.

关 键 词:计算流体力学  欧拉运动方程  可压缩流动  非结构网格  推进阵面法  有限体积法
文章编号:
收稿时间:1998-10-14

Generation of the 2D Unstructured Grids and the Euler Solution on It
WANG Ping,ZHU Zi-qiang. Generation of the 2D Unstructured Grids and the Euler Solution on It[J]. Journal of Beijing University of Aeronautics and Astronautics, 2000, 26(2): 190-193
Authors:WANG Ping  ZHU Zi-qiang
Affiliation:Beijing University of Aeronautics and Astronautics,Dept. of Flight Vehicle Design and Applied Mechanics
Abstract:Computational unstructuredgrid is generated by advancing front method, and the structured background gird isobtained by using multigrid technique to solve the Poisson equation. A new method ofboundary discretization is presented for generating the initial fronts, and a novel datastructure—Array Linked List is proposed to store the grid data. The Euler equations onunstructured grid are solved by cell-centered scheme of finite volume method. Numericalexamples show that the correlation of the computational results with experimental data isfavorable and the need of N-S equations solver is obvious for both case of airfoil intransonic flow and multi-element airfoil in subsonic flow.
Keywords:computation fluid mechanics  Euler motion equations  compressible flow  unstructured grid  advancing front method  finite volume method
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