aerofoil
基本解釋
- n.翼型；翼剖面；機翼
英漢例句
- With use of this structure model, we can simulate the real performance of aerofoil very well.
應(yīng)用該結(jié)構(gòu)模型可以很好的模擬機翼結(jié)構(gòu)的實際情況。 - The author modifies spanwise shape and makes the analog function of the aerofoil curve by use of the computer.
利用計算機來輔助葉片葉展形狀的修正和構(gòu)造翼型曲線的模擬函數(shù)。 - Three kinds of fan blade aerofoil have been designed according to the velocity distribution optimization criterion.
并依據(jù)探索出的速度分布優(yōu)化準(zhǔn)則,設(shè)計出了三種風(fēng)機葉片的翼型。 - Some exemples to apply the aerofoil computed from these formula to the fan design are listed. ?
并列舉了利用其公式算出的翼型在風(fēng)機設(shè)計上的應(yīng)用實例。 - Aerofoil impeller is a new kind of axial flow impeller,which has high mixing performance in reaction vessel.
翼型槳是新一代高效槳葉。
詞組短語
- aerofoil lift 氣翼上升;風(fēng)翼升力
- aerofoil blade 葉片
- aerofoil effect 機翼效應(yīng)
- aerofoil shape 翼型形狀
- isolated aerofoil 孤立翼型
短語
英英字典
- a cross section of an aileron, wing, tailplane, or rotor blade ,,,
柯林斯英英字典
專業(yè)釋義
- 機翼
- 翼型
Results show that the Cl/Cd rises when Gurney flaps are attached to the aerofoil,and the lift force tend to distribute more reasonably. The high-est Cl/Cd is got when the height of Gurney flap is 3%C.
計算結(jié)果表明,安裝Gurney襟翼后翼型的升阻比得到提高,升力分布趨于平均,在所計算的氣流條件下安裝3%C高度Gurney襟翼的翼型獲得了最高的升阻比。 - 翼剖面
- 翼切面
- 翼型
Changing the mount angle of the impeller aerofoil in a centrifugal pump to eliminate eddy entirely.3.
2．改變?nèi)~輪翼型安放角度，進(jìn)一步消除旋渦。 - 翼面
- 空氣動力面
- 機翼
- 翼型