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.
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 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.
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。
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.
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。
CHORD - distance from leading to trailing edge of a wing.
弦—从机翼前缘到尾缘的距离。
AILERON, a hinged moveable part on the trailing edge of each wing for airplane roll (wing up and wing down) control.
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)。
A section of (wing trailing-edge) flap detached during flight probably due to material fatigue.
一段襟翼在飞行中掉落可能因材料疲乏。
Conventional trailing-edge wing flaps help delay the stall to a higher lift coefficient, but only with limited effectiveness.
传统的后缘襟翼有助于延缓失速到一个更高的升力系数，但只有有限的成效。
For example, the trailing edge of the wing is relatively shallow.
例如，大翼后缘的厚度相对较薄。
A hinged moveable part on the trailing edge of each wing for airplane roll (wing up and wing down) control.
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)。
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.
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。
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.
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。
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.
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。
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。
The upper surface can have an intersection point with the wing when the trailing edge device is in the stowed position.
上表面在后缘装置处于收回位置时与机翼有一交汇点。
And the viscous separation flow of wing-body trailing edge conjunction can be effectively simulated. Therefore these algorithms are valuable for the engineering applications.
计算结果与风洞实验的对比表明，文中所采用的数值方法可以有效的模拟翼身结合处粘性分离流动，具有一定的工程实用价值。
And the viscous separation flow of wing-body trailing edge conjunction can be effectively simulated. Therefore these algorithms are valuable for the engineering applications.
计算结果与风洞实验的对比表明，文中所采用的数值方法可以有效的模拟翼身结合处粘性分离流动，具有一定的工程实用价值。
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