1、Transformative problem of aerofoil impeller is put forward.
提出了機(jī)翼型葉輪的改造問題。

2、It may obtain a special experiment aerofoil lift-drag force characteristic with this test.
通過本實(shí)驗(yàn)，可以測(cè)得某一特定實(shí)驗(yàn)機(jī)翼的升力特性和阻力特性。

3、Optimal design on aerofoil parameter of impeller is made based on the second YQH-100 oil-gas pump.
基于第二代YQH-100油氣混輸泵葉輪的基本參數(shù)，對(duì)葉輪的翼型參數(shù)進(jìn)行了優(yōu)化設(shè)計(jì)。

4、Profile Correction for the Blade of a Diagonal Flow Aerofoil Impeller
翼型斜流葉輪的葉形修正方法

5、The rotor blades work like the wings of an aeroplane, with an aerofoil shape providing lift.
旋轉(zhuǎn)葉片的工作原理類似飛機(jī)的兩翼，運(yùn)用機(jī)翼的形狀提供上升力。

6、With use of this structure model, we can simulate the real performance of aerofoil very well.
應(yīng)用該結(jié)構(gòu)模型可以很好的 * 翼結(jié)構(gòu)的實(shí)際情況。

aerofoil翻譯