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.

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。

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。

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)

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。

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。

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.

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.

Also called Tail edge, Trailing edge.

故有圆筒尾, 版尾和纸尾的名称.

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.

The movement occurs on the trailing edge of the pulse.

移动是在脉冲的下降沿产生的.

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.

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.

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

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.