The movement occurs on the trailing edge of the pulse.
移动是在脉冲的下降沿产生的。
The movement occurs on the trailing edge of the pulse .
移动是在脉冲的下降沿产生的。
CHORD - distance from leading to trailing edge of a wing.
弦—从机翼前缘到尾缘的距离。
For example, the trailing edge of the wing is relatively shallow.
例如，大翼后缘的厚度相对较薄。
The trailing edge of the second pulse, therefore, also ACTS as an event horizon.
因此，第二个脉冲的后缘地带也发挥了视界的作用。
As mentioned in the definitions section ks is the trailing edge thickness parameter.
如上定义组是皇尾缘厚度参数。
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。
The invention relates to a device for positioning the trailing edge of sheets in a blade folder.
本发明涉及用于定位优选在组合式折页机中运动的页张的装置。
Interesting values may be expected from the trailing edge the profile centre and the leading edge.
从后缘，叶型中心和前缘可预料得到有价值的数据。
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。
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。
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)。
Attribute 2. The attribute to be constrained on the second item-in this case, the blue view's trailing edge.
对第二项进行限制的属性2 - - -在这里是指蓝色视图的右边界。
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。
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。
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 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。
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。
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)。
That has some signature implications, with what looks like an almost unswept trailing edge, because edges scatter forward and backwards.
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。
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。
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。
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。
The heat transfer and characteristics of the fluid flow in the duct of the trailing edge of the turbine blade with parted pin-fin arrays were experimentally investigated.
本文对具有断裂结构扰流柱的涡轮叶片尾缘楔型通道的流动与换热过程进行了实验研究。
The heat transfer and characteristics of the fluid flow in the duct of the trailing edge of the turbine blade with parted pin-fin arrays were experimentally investigated.
本文对具有断裂结构扰流柱的涡轮叶片尾缘楔型通道的流动与换热过程进行了实验研究。
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