： 中文名称：翼载荷 英文名称：wing loading 翼载荷是指飞机重量和机翼面积之比。通常说的翼载荷是指起飞时的翼载荷，即起飞重量和机翼面积之比。翼载荷是飞机总体设计的主要参数之一，关系着飞机的起降性能、爬
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missile wing load emulation sys-tem 弹翼负载模拟系统
ultimate-load wing-up bending test 机翼极限载荷测试
Wing sideways static load test 护翼侧向静载测试
The paper introduces the difficulties met in A/C loads calculation during abrupt pitching maneuver and rolling pullout, and in wing load calculation during rolling maneuvers.
介绍在使用国军标规范《军用飞机强度和刚度规范》中对于急剧俯仰机动、滚转改出及滚转机动机翼载荷计算时所遇到的困难、解决办法及其软件研制。
The final test occurred Apr. 21 when the wing and trailing edges were subjected to their limit load of around 2.5g, the highest loads expected to be seen in service.
根据4月21最终试验的结果，机翼和后缘的承受的极限负荷为2.5g左右，而实际最高负荷只能在实际服役的时候才能知道。
As an example of large sized structural component, the mechanical model of load calibration test of an airplane wing was analysed.
以飞机机翼等大型结构为例，探讨了大型结构部件载荷标定试验的力学模型。
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