本文采用面搭接网格技术成功解决了传统点对点连接网格技术模拟涡流发生器流动网格数量过大的问题；

Using patched grid technique, this article successfully solves the problem of massive grid number caused by using conventional point-to-point gird.

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研究也表明，面搭接网格生成技术在研究高升力构型这类复杂外形流动问题时，同样可以保证较高的数值模拟精度。

The research also shows that, patched grid technique can, as well, achieve good numerical accuracy at dealing with complicated configurations such as high lift system.

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