本文给出了一种多段翼型绕流的分区贴体网格生成方法。
A method has been developed which generates the body-fitted coordinates of multi-element airfoils by using of a grid patching technique.
计算中使用了贴体坐标数值网格生成方法。
Body fitted grid generation method is employed for the computation.
为了提高网格最终生成质量，内部节点定位是采用扫掠法生成六面体网格过程中的关键一步。
In order to improve the final mesh quality, placement of interior nodes is a crucial step in the generation of hexahedral meshes using sweeping algorithms.
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