摘要
基于Jameson的有限体积方法,采用多块网格技术求解Reynolds平均N-S方程组,对三维增升装置绕流进行数值模拟。提出了新颖的嵌补式多块网格技术,使得网格生成和流场计算得到了明显的简化。计算结果与实验数据吻合良好。
There are great difficulties in numerical simulation of flow about 3D liften hancing device , both in grid generation and flow field solving. This paper pres ents a novel MultiBlock Grid Technology-the so called Embedding Grid Technolo gy, which provides a simple way to solve this problem. In this method, the ideas of Chimra grid and Patch grid are combined. The grids of components, such as fl aps and slats, are embedded in assigned windows of main wing grid. The grid gene ration and programming of flow solver are both dramatically simplified.The conse rvative information exchanges are executed on boundaries of windows, which are c ommon interfaces of component and main grids. As a validation, flow field about a wing with a half span flap is computed with the present method. Results ar e in good agreement with experiment data. Much fewer grid blocks, with the prese nt method than with traditional Patched Grid Technology, are demanded.
出处
《空气动力学学报》
CSCD
北大核心
2003年第1期90-97,共8页
Acta Aerodynamica Sinica
基金
航空基础科学基金资助(98A53005)
博士后基金资助.
关键词
三维增升装置
嵌补式网格技术
多块网格
守恒
N-S方程组
3-D lift-enhancing device
embedding grid technology
multi-block grid, conse rvation
N-S equations