leading edge airfoil surface
基本解释
- 前缘翼面
英汉例句
- 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。
ip.com - The stall of the wing occurs at the highest lift coefficient on an airfoil, when the airflow can no longer go around the airfoil's nose (leading edge) and separates from the upper wing surface.
机翼失速的发生在电梯表面系数最高的机翼上，当气流不能继续围绕翼型的鼻子（领先），并脱离机翼上。