基本解釋

英漢例句

The leading edge portion includes a plurality of staggered holes for causing fluid to flow over a surface of the airfoil portion.
該前緣部包括多個(gè)錯(cuò)開的孔以便使流體在該翼面部的表面上流動(dòng)。
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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.
機(jī)翼失速的發(fā)生在電梯表面系數(shù)最高的機(jī)翼上，當(dāng)氣流不能繼續(xù)圍繞翼型的鼻子（領(lǐng)先），并脫離機(jī)翼上。