该前缘部包括多个错开的孔以便使流体在该翼面部的表面上流动。
The leading edge portion includes a plurality of staggered holes for causing fluid to flow over a surface of the airfoil portion.
该前缘部包括多个错开的孔以便使流体在该翼面部的表面上流动。
The leading edge portion includes a plurality of staggered holes for causing fluid to flow over a surface of the airfoil portion.
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