wing loading

The task of the initial sizing is to find the primary parameters of aircraft, including the takeoff wing loading, thrust-to-weight ratio, takeoff weight, wing area, aspect ratio of wing, wing sweep, thickness and taper ratio to match the mission requirements.

其任务是找到能满足飞机性能要求的飞机主要参数。这些参数包括：起飞翼载、推重比、起飞重量、机翼面积、机翼翼载、机翼后掠角、机翼相对厚度和机翼梯形比等。

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This paper studies the design and the realization of missile's wing and rudder load simulation system based on DSP ( Digital Signal Processor) and DTC ( Direct Torque Control) servo driver after introducing the basic principles of electric loading system.

本文在分析电动加载系统基本原理的基础上，研究了以数字信号处理器（DSP）和具有直接转矩控制输出的ACS600伺服驱动器为核心的弹用加载控制系统的设计及实现方法。

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In the carpet plot module, the relation of the aircraft takeoff weight with the wing loading and thrust-to-weight ratio are displayed on the carpet plot, and various requirement boundaries are also plotted on the same plot.

在地毯图中，描述了飞机推重比和翼载与客机最大起飞重量之间的相互关系。同时依据界限线的绘制方法，也将客机各个设计性能要求绘制在同一张图上。

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In the sizing diagram, the boundaries of different performance requirements are plotted as functions of the wing loading and thrust-to-weight ratio.

界限线图上的每条界限线都描述了不同的飞机性能要求下的翼载和推重比之间的关系。

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By using this carpet plot, a designer can conveniently select the values of the wing loading and the thrust-to-weight ratio to minimize the takeoff weight, while still meeting the performance requirements.

通过地毯图，设计人员可以选取在满足飞机各个设计性能要求约束下使得飞机起飞重量最小的推重比和翼载的组合。

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