trailing edge

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.

词典精选例句

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。

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And the trailing edge has a flexible fringe, unlike the rigid trailing edge of a conventional bird wing.

而接下去的尾端则是一小段柔韧的弯曲，不像是一般的羽翼末端那样坚硬。

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And also there are two kinds of the trailing edge, concave and oblate spheroid.

气泡的尾部形状也分为两种：凹形和扁球形。

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How wire measurements of trailing edge boundary layer and near wake flow characteristics of a low speed airfoil

低速翼型近场尾流及其后缘边界层流动特性之热线测量结果

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adult: tail unbarred pale rufous above, slightly paler and greyer below; broad black band along trailing edge of wing.

成鸟：尾羽上部淡棕色，无条纹，下部稍淡而发灰，翼外缘有宽的黑色镶边。

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Also called Tail edge, Trailing edge.

故有圆筒尾, 版尾和纸尾的名称.

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this paper aims at presenting an investigation into aerodynamics and control reversal characteristics of adaptive wings with seamless, variable camber, flexible trailing edge.

对后缘可无缝、连续柔性偏转的自适应机翼进行了二元气动特性和操纵反效特性分析。

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Leading edge and trailing edge means the function of the dimmer.

飞机螺旋桨的前边缘和机翼后边缘是最能够反应调光器的功能的.

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The movement occurs on the trailing edge of the pulse.

移动是在脉冲的下降沿产生的.

词典精选例句

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.

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the transition from voltage to no voltage is referred to as the trailing edge of a clock signal.

电感从一定值下降到0值的跃迁叫做时钟信号的后沿。6.Insider: What sort of challenges are there in this artistic transition from The Burning Crusade to Wrath of the Lich King?那么，从燃烧远征到巫妖王之怒的艺术风格过渡里，将有些什么样的挑战呢？。

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Trailing edge of fork crown and frame down tube present a virtual continuous surface to the wind. reducing aerodynamic drag.

前叉肩部的延伸边缘和车架的下管形成一个虚拟的连续迎风面，从而有效地减少风阻。

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ⅳ region is trailing edge vortex region of tip near the flange of blade.

Ⅳ区为叶片出水边靠尾部的轮缘出口尾涡区。

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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.

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the effect of different clapboards structure in turbine blade trailing edge complex passages on heat transfer characteristics

涡轮叶片尾缘复合通道中隔板结构对换热特性的影响

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In order to investigate the flow characteristics of cooling flow downstream of a turbine guide vane trailing edge slot, numerical methods of RNG k-ε turbulent model were solved.

通过RNG k-ε湍流模型求解可压流的N-S方程，研究燃气轮机涡轮导向叶片尾缘劈缝出流冷气的流动情况。

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This article experimentally studies the effects of air injection near the blade trailing edge on flow separation and losses in a highly loaded linear compressor cascade.

对应用射流孔的高负荷压气机直叶栅进行了实验研究，着重研究了孔隙射流对削弱尾缘附近流动分离和损失的效果。

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In addition, trailing edge symmetrical jet has little influence on the position of the vortex axis.

另外, 后缘对称喷流对涡轴位置的影响很小.

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Trailing edge blowing wake management technology was adopted to improve the flow of stator wake.

采用尾缘吹气的流动控制技术,改善静子尾迹区流动.

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Numerical simulation effect of modified trailing edge on airfoil flow field

改型尾缘对翼型流场影响的数值模拟

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A move of the centre of pressure towards the trailing edge.

压力中心向尾部移动(译者注:实际是翼型改变了, 焦点力矩增大了)

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A numerical study of aerodynamic characteristics of modified aerofoil with a blunt trailing edge

翼型进行钝尾缘修改后气动性能的数值研究冲压式翼伞后缘下拉气动特性的数值研究

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On the bases of the analytical results of deformation and stress fields, some concise formulae to calculate the thrust distance of the overlying thrust sheet and the force existing on the trailing edge of the sheet while decoupling are given.

利用变形场与应力场的分析结果，给出了推覆构造在拆离时推覆席体的推移距离及作用推力的简捷计算公式。

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By modifying the thickness of the blade trailing edge, research influences of the blade trailing edge to the aerodynamic performance and noise levels.

通过修改叶型尾缘厚度，研究叶型尾缘厚度对风洞风扇的气动性能和噪声水平的影响。

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For recognition, the front or trailing edge of projection of binary image on horizontal axis basically shows linear shape, so least square theory is applied in tilt correction.

识别过程中，数码管二值化后的图像在水平轴上的投影，其上升沿或下降沿基本呈现直线的形状，尝试把最小二乘法应用于倾斜校正。

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With help of experiment and CFD simulations, character of tip vortex and trailing edge vortex of partly-ducted axial flow fan is studied, with flow change in outdoor units also analyzed. 2.

实验结果结合三维CFD数值模拟研究了部分管道式轴流风扇系统叶尖涡、尾缘涡特征，及其在室外机内部的流动变化。

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In accordance to analysis of interaction mechanism between the ejection and the main flow, a 2-D compressible model of the turbine blade trailing edge ejection has been improved, which uses energy loss coefficient for representing the effect of the ejection on the aerodynamics of the main flow.

本文分析了叶片尾缘喷气与主流干扰的机理，改进了二维、可压缩的涡轮叶栅尾缘喷气模型，并以能量损失系数ξF来反映冷气喷射对主流的气动影响。

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Finally, the wing is coated with RAM at its leading edge and trailing edge.

在此基础上, 对机翼前后缘局部涂敷吸波材料.

网络文摘精选

A Subject "Impact of Suction Surface Shape on High Pressure Turbine Trailing Edge Loss" has been conducted by BRR, GTE and DLR.

由德国宝马·罗·罗（BRR）、中国燃气涡轮研究院（GTE）和德国宇航院（DLR）联合开展了叶背表面曲率的变化对高压涡轮尾迹损失的研究。

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