TED：后缘向下

“Trailing Edge Down”在技术文档或专业交流中常被缩写为TED，这种简写方式便于快速记录和使用，尤其在美国航空航天局（NASA）等航空航天机构中应用广泛。该术语的中文释义为“后缘向下”，通常用于描述飞行器机翼或控制翼面的后缘向下偏转的特定姿态或状态。

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。
When one row on one side blows air at a higher pressure than the other it causes the airflow over the trailing edge on that side to bend up or down, in exactly the way that an aileron would, and the plane rolls accordingly.
当一侧机翼上的一排狭槽喷出的空气压力大于另一排，就导致了掠过机翼后缘的气流偏向上方或偏向下方，与副翼的作用完全相同，飞机随之上升或下降。
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）。
The trailing-edge loss of radial inflow turbine stator was discussed based on the loss models of NASA, showing that the loss increases linearly with the trailing edge thickness. Thus, an efficient method of reducing trailing-edge loss is to cut down the trailing edge thickness.
基于NASA损失模型分析了径向透平静叶的尾缘损失，损失随着出口边厚度呈线性增加，减小出口边厚度是减小尾缘损失的有效方法。

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