副翼是机翼后缘的可动部分。
The ailerons are movable sections along the rear edges of the wings.
一群地勤人员冲向前去，抓住了机翼后缘上的特殊套环。
A handling party rushed forward and grabbed hold of special toggles on the trailing edges of the wings.
本方法的特色是改进了机翼表面网格点的分布，使机翼后缘与网格线一致。
The method presented has the feature that the trailing wing edge is aligned with the grid line through modification of the distribution of the mesh points on the wing surface.
铰连在每个机翼后缘的可动部件，用于控制飞机的滚转(机翼向上和向下)。
A hinged moveable part on the trailing edge of each wing for airplane roll (wing up and wing down) control.
提出在垂直极化状态下机翼后缘绕射的计算必须将后缘厚度考虑在内的见解。
The scattering peak of leading edge depends only on radius of airfoil for horizontal polarization.
副翼，铰连在每个机翼后缘的可动部件，用于控制飞机的滚转(机翼向上和向下)。
AILERON, a hinged moveable part on the trailing edge of each wing for airplane roll (wing up and wing down) control.
这里有些特征性暗示，看上去机翼后缘几乎没有清理过，因为有些翼缘前后散开着。
That has some signature implications, with what looks like an almost unswept trailing edge, because edges scatter forward and backwards.
我们发现不需要可变形机翼后缘概念，尽管那是AFRL的传感飞行器设计概念之一。
We found we didn't need a flexible trailing edge concept, although this was one of the AFRL ideas for SensorCraft.
第二架原型机的机翼后缘、其他结构部件和系统正在组装。第三架原型机的第一个结构段已经完成。
The second prototype's wing trailing edge and other structural components and systems are being assembled and the first structural segments of the third prototype are being finished.
襟副翼有自己的翼型，并挂在机翼后缘下方新鲜空气原状的速度控制在较低的最大效益，甚至他们与供应。
The flaperons have their own airfoil, and are hung below the wing trailing edge to supply them with fresh undisturbed air for maximum control effectiveness even at low speeds.
实验室的研究表明，它已经成了机翼的一项功能，也是通过适形机翼后缘表面来增强层流的流控制技术的功能。
Looking at that in the lab, it becomes a function of airfoil shape, and also of the flow control technologies you use to enhance the laminar flow with conformal trailing edge surfaces.
风洞实验采用PIV测量了沿流向下游不同截面的涡量场和速度场，测量截面距机翼后缘最远达到20倍弦长。
Wind tunnel measurement gives the velocity field and vorticity field in intersection plane at different downstream position, which is up to 20 times cord-length.
根据4月21最终试验的结果，机翼和后缘的承受的极限负荷为2.5g左右，而实际最高负荷只能在实际服役的时候才能知道。
The final test occurred Apr. 21 when the wing and trailing edges were subjected to their limit load of around 2.5g, the highest loads expected to be seen in service.
与今天使用的典型机翼相比，SUGARVolt的机翼的翼尖相距更远，前缘与后缘之间相距更短，并且后掠角更小。
Compared to the typical wing used today, the SUGAR Volt wing is longer from tip to tip, shorter from leading edge to trailing edge, and has less sweep.
其他的研究人员把研究焦点集中在机尾乱流的源头上，就是机翼的后缘。
Other researchers are focusing on the source-the trailing edges of aircraft wings.
你是否注意过当飞机在水平状态时，机翼的前缘要比后缘高？
Have you ever noticed that when an airplane is level, the front edges of its wings are higher than the rear ones?
本文简要地阐述了具有后缘控制面的二元机翼模型主动颤振抑制低速风洞试验的全过程。
This paper gives a brief description of the whole process of the low-speed wind tunnel test for active flutter suppression of a two-dimensional wing model with trailing edge control surface.
连接机翼的前缘与后缘的直线。
A straight line connecting the leading and trailing edges of an airfoil.
然而板条，结合边缘皮瓣与领先使用的后缘，机翼的升力系数，可有效地增加一倍，如果用在机翼完整的跨度。
However, by combining the use of trailing-edge flaps with leading-edge slats, the wing's lift coefficient can be effectively doubled if used on the full span of the wing.
上表面在后缘装置处于收回位置时与机翼有一交汇点。
The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position.
建立了带柔性后缘自适应机翼模型和带刚性偏转后缘的传统机翼模型，从升阻特性和力矩特性以及操纵效率对它们进行了比较研究。
This paper aims at presenting an investigation into aerodynamics and control reversal characteristics of adaptive wings with seamless, variable camber, flexible trailing edge.
次要结构由机翼前缘，后缘和翼尖构成，主要用来减小空气阻力，支撑蒙皮，协助飞行操纵面和操纵机构。
The secondary structures, which support aerodynamic fairings or skins, flight control surfaces and control mechanisms, consist of the leading edge, trailing edge, and wingtip.
本文针对后缘变弯度机翼，设计出一种新的柔性蜂窝结构。
In this article, a new flexible honeycomb structure is designed for the wing with a variable camber trailing edge.
本文针对后缘变弯度机翼，设计出一种新的柔性蜂窝结构。
In this article, a new flexible honeycomb structure is designed for the wing with a variable camber trailing edge.
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