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。
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)。
ELEVATOR, a hinged moveable part on the trailing edge of the horizontal stabilizer for airplane pitch (nose up and nose down) control.
升降舵，铰连在水平安定面后缘上的可动部件。用以操纵飞机的俯仰运动(机头朝上及朝下)。
CHORD - distance from leading to trailing edge of a wing.
弦—从机翼前缘到尾缘的距离。
It also constrains the view's trailing edge relative to the superview's trailing edge.
它还约束了视图相对于父视图的结束边界。
Returns the rectangle for the leading or trailing edge of the character at the specified index.
返回指定索引处字符的前边缘或后边缘的边框。
Heat transfer in channel for trailing edge of turbine blade with pin-fin arrays is studied numerically.
对涡轮叶片尾缘针肋通道的换热进行了数值模拟研究。
Numerical methods are used to investigate the film cooling effect of turbine guide vane's trailing edge.
采用数值模拟的方法，研究了涡轮叶片尾缘斜劈缝气膜冷却的流场特性，及其对叶背面尾缘温度分布的影响。
Aircraft trailing edge devices, including devices with non-parallel motion paths, and associated methods.
飞行器后缘设备，含运动路径非平行的设备，和有关方法。
A high suction peak is induced by the stall vortex as the trailing edge vortex sheds downstream smoothly.
后缘涡顺利地从后缘脱落时，失速涡在上翼面能诱导出较大的吸力。
They have carbon-fiber top and bottom skins, sides and a trailing edge profile, bonded to a honeycomb core.
其内部是蜂窝结构，上下碳纤维表面、侧边以及后缘与蜂窝结构粘接在一起。
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)。
BALANCE TAB, a small hinged moveable part on the trailing edge of a control surface (aileron, elevator, rudder).
随动补偿片，铰接在操纵面后缘(副翼，方向舵，升降舵)的可动部。
The position of the trailing edge can then be calculated based on the superview's size and the other constraints.
结束边界的位置可以根据父视图的尺寸计算出来，其它约束也是。
We found we didn't need a flexible trailing edge concept, although this was one of the AFRL ideas for SensorCraft.
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。
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。
A numerical study has been performed for the condensing flows in a cascade, which has five different trailing edge shapes.
本文对一个叶型五种出气边形状对应的凝结流动进行了比较，以初步揭示几何参数影响凝结流动的机理。
Abstract: The traditional BPM semi-empirical prediction airfoil turbulent boundary layer trailing edge noise was improved.
摘要：改进了传统的翼型湍流边界层尾缘噪声bpm半经验预测公式。
Aim To study the movement regularity of homogeneous soil landslide with known trailing edge and undetermined shear opening.
目的研究均质土体滑坡(已知后缘裂缝位置，未知前缘剪出口位置)运动规律。
The system becomes overdetermined as zero vortex strength is set at trailing edge, to make the Kutta condition be satisfied.
为满足库塔条件而令后缘处涡强度为零，但导致了方程组的矛盾性。
Aircraft trailing edge devices, including devices having forwardly positioned hinge lines, and associated methods are disclosed.
本发明涉及一种飞机后缘装置，包括具有位于前端的铰接线的装置以及相关方法。
In this thesis, the control law based on adaptive filter for Smart Rotor with actively controlled trailing edge flap is researched.
本文主要研究基于自适应滤波的主动控制后缘附翼智能旋翼控制律设计问题。
In this paper, heat transfer and fluid flow in passage for trailing edge of turbine blade with pin-fin arrays is studied numerically.
本文应用湍流模型对涡轮叶片尾缘针肋通道的换热与流动进行了二维数值模拟研究。
The leading edge of the buffer has a mobility equal to or less than the surfactant, whereas the trailing edge has a mobility close to water.
流度缓冲液的前缘的流度等于或小于表面活性剂的流度，而它的后缘的流度接近于水的流度。
The numerical study was carried out on the trailing edge cooling of turbine blade using the circular pin fin that was arranged in cross type.
对一个有交叉排列圆形扰流柱的涡轮叶片尾缘冷却方案进行了数值研究。
The ejection from the half slot only blows away the vortex on the slot surface, and has little effect on the flow field near the trailing edge.
半开缝时，喷气的引入仅吹除了附着在开缝处的漩涡，对于尾缘处流场影响不大。
The computations show that the droplets distribution, entropy increase, wetness fraction, and flow angle are changed when the shape of trailing edge varies.
结果显示，出气边形状的改变影响凝结流中水滴状态、熵增、湿度、出口气流角的分布。
It is shown that in the present numerical investigations, the trailing edge shape and the reduced frequency have an important influence on the vortex evolution.
数值研究表明，后缘形状、折合频率等对涡结构演化有重要影响。
It is shown that in the present numerical investigations, the trailing edge shape and the reduced frequency have an important influence on the vortex evolution.
数值研究表明，后缘形状、折合频率等对涡结构演化有重要影响。
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