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trailing edge flaps

Vertaling van "trailing edge flaps" in Chinees

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后缘襟翼
The trailing edge flaps can be operated with the alternate electrical system.
可以用备用电源操纵后缘襟翼。
To utilize trailing edge flaps, and thus increase the maximum lift coefficient, the wing must go to a higher angle of attack without airflow separation.
为利用后缘襟翼,因此增加最大升力系数,机翼必须迎角更大而没有气流分离。
To configure for a landing with trailing edge flaps less than 1.
后缘襟翼小于1时完成着陆构型。
The pointed leading edge necessary for high-speed flight results in an abrupt stall and restricts the use of trailing edge flaps because the airflow cannot follow the sharp curve around the wing leading edge.
尖角的前缘对于高速飞行必定导致突然失速,限制后缘襟翼的使用,因为气流不能沿机翼前缘的尖锐曲线流动。
trailing edge flaps are in a skew or asymmetry condition, or have uncommanded motion, or
后缘襟翼不一致或不对称,或者不在指令位置,或
Secondary or auxiliary flight controls include tabs, leading edge flaps, trailing edge flaps, spoilers, and slats.
辅助飞行控制包含配平片,前缘襟翼,后缘襟翼,扰流板以及前缘缝翼(slat)。
As is true with trailing edge flaps, a small increment of leading edge flaps increases lift to a much greater extent than drag.
相比后缘襟翼来说,前缘襟翼的一点增量会让升力比阻力增加多的多。
The leading edge devices fail to extend and trailing edge flaps are less than 1.
前缘装置不能放出并且后缘襟翼小于1。
The trailing edge flaps are not symmetrically extended.
后缘襟翼不对称放出。
Therefore, the sections of the wind turbine blade with the morphing part 12 and the trailing edge flap 13 will have to compensate for the variations of loads (forces and moments) in the sections with no morphing parts 12 or trailing edge flaps 13.
因此,风轮机叶片的具有变形部12和后缘襟翼13的那些区段必须补偿不具有变形部12或后缘襟翼13的那些区段的负载(力和力矩)的变化。
Leading edge flaps, like trailing edge flaps, are used to increase both CLmax and the camber of the wings.
前缘襟翼类似后缘襟翼,用来既增加最大升力系数有增加机翼的曲面弯度。
Do not attempt to move the trailing edge flaps with the ALTERNATE FLAPS switch because there is no asymmetry protection.
因为没有不对称保护,不要试图用备用襟翼电门移动后缘襟翼。
Trailing edge flaps normal hydraulic system inop
后缘襟翼正常液压系统不工作
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Synoniemen voor trailing edge flaps in het Engels

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