翼载

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。

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

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。

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 .

设计变量为导弹的推重比、翼载和被动段的比例导引系数。

Variables are the thrust to gravity ratio ; the load of wing ; proportional coefficient in passive trajectory .

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。

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 .

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。

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 .

研究结果揭示了联接翼结构受载特点，分析了其高结构效率的根本原因。

The result of this research reveals the structural characteristics and the reason of high structural efficiency of joined wing .

大展弦比连接翼飞机考虑预载作用下的非线性模态与颤振特性研究

Analysis of the nonlinear modal and flutter characteristic for HAR Joined wing considering the prestressing force