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。
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.
在燃烧器区域处使网格线与煤粉射流方向基本一致，以有效地减小数值模拟中的伪扩散问题。
The direction of grid lines in the burner block is consistent with the direction of pulverized coal jet, which can reduce false diffusion in the simulation.
在燃烧器区域处使网格线与煤粉射流方向基本一致，以有效地减小数值模拟中的伪扩散问题。
The direction of grid lines in the burner block is consistent with the direction of pulverized coal jet, which can reduce false diffusion in the simulation.
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