计算物理 ›› 2002, Vol. 19 ›› Issue (4): 362-366.

• 论文 • 上一篇    下一篇

多段翼型粘性绕流多块网格数值模拟

陈海昕1, 李凤蔚2, 鄂秦2, 肖志祥2   

  1. 1. 清华大学工程力学系, 北京 100084;
    2. 西北工业大学飞机工程系, 陕西 西安 710072
  • 收稿日期:2001-01-20 修回日期:2001-05-10 出版日期:2002-07-25 发布日期:2002-07-25
  • 作者简介:陈海昕(1974-),男,湖南隆回,博士后,主要从事计算流体力学研究.
  • 基金资助:
    航空基础科学基金资助项目

NUMERICAL SIMULATION OF VISCOUS FLOW FOR MULTI-ELEMENT AIRFOIL USING MULTI-BLOCK GRIDS

CHEN Hai-xin1, LI Feng-wei2, E Qin2, XIAO Zhi-xiang2   

  1. 1. Department of Engineering Mechanics, Tsinghua University, Beijing 100084, China;
    2. Department of Aircraft Engineering, Northwestern Polytechnical University, Xi'an 710072, China
  • Received:2001-01-20 Revised:2001-05-10 Online:2002-07-25 Published:2002-07-25

摘要: 采用多块结构网格和分区求解技术对多段翼型绕流进行雷诺平均NS方程数值模拟,并将计算的压力分布与实验进行了比较.

关键词: 多块网格, 点对点搭接, 多段翼型

Abstract: Grid generation and flow analysis methods for multi-element airfoil based on multi-block point-to-point patched grid technology are developed. Some strategies are developed to improve the efficiency, accuracy and applicability of the method.Several flow cases about multi-element airfoils are computed with the present method in order to validate it. Numerical results are in agreement with experiment data. Flow field visualization shows that the present method has good resolution in flow details.

Key words: multi-block grid, point-to-point patch, multi-element airfoil

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