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翼-身组合体的网格生成与N-S方程数值模拟
引用本文:胡勇军,税清才,匡赢,王国镔. 翼-身组合体的网格生成与N-S方程数值模拟[J]. 贵州大学学报(自然科学版), 2010, 27(6): 117-119,123
作者姓名:胡勇军  税清才  匡赢  王国镔
作者单位:贵航飞机设计研究所,贵州,安顺,561000;贵航飞机设计研究所,贵州,安顺,561000;贵航飞机设计研究所,贵州,安顺,561000;贵航飞机设计研究所,贵州,安顺,561000
基金项目:贵州省科技厅科技计划项目
摘    要:以DPW4的CRM模型为例,给出了一种复杂外形飞行器网格生成的分块对接网格拓扑方案以及实现过程,在无限插值法生成的初始网格基础上,用椭圆微分方程生成空间网格。基于该网格求解N-S方程,获得了较为合理的全机气动力系数与压力分布。

关 键 词:飞机  分块网格  计算流体力学  N-S方程

Grid Generation of Wing-fuselage Configuration and Value Simulation of N-S equations
HU Yong-Jun,SHUI Qing-Cai,KUANG Ying,WANG Guo-Bin. Grid Generation of Wing-fuselage Configuration and Value Simulation of N-S equations[J]. Journal of Guizhou University(Natural Science), 2010, 27(6): 117-119,123
Authors:HU Yong-Jun  SHUI Qing-Cai  KUANG Ying  WANG Guo-Bin
Affiliation:(GAIC Aircraft Design and Research Institute,Anshun 561000,China)
Abstract:Taking CRM model of DPW4 as an example,and a topology project and the realization process for multi-block patched grid were given to generate the grid of A/C with complicated shape.On the basis of initialization grid generated by TFI method,the spatial grid was generated with elliptic differential equation.And N-S equations was solved on the basis of the grid for obtaining the reasonable aerodynamic coefficients and pressure distribution of whole A/C.
Keywords:A/C  block grid  computational fluid mechanics  N-S equations
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