The method presented has the feature that the trailing wing edge is aligned with the grid line through modification of the distribution of the mesh points on the wing surface.

本方法的特色是改进了机翼表面网格点的分布，使机翼后缘与网格线一致。

youdao

The method presented has the feature that the trailing wing edge is aligned with the grid line through modification of the distribution of the mesh points on the wing surface.

本方法的特色是改进了机翼表面网格点的分布，使机翼后缘与网格线一致。

youdao