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1·To test this algorithm, one design example, one rib of an aircraft wing, is given.

为验证该算法，给出了一个飞机水平安定面翼肋设计实例。

2·The paper analyzes the external stores jam flutter characteristics of aircraft wing.

分析了飞机机翼—外挂干扰颤振特性。

3·A new kind of modelling was proposed on aircraft wing structural analysis and optimization.

提出一种新的飞机翼面结构分析和优化的建模技术。

4·The second half of the paper presents the research of the layout optimization of aircraft wing .

后半部分利用近似技术对飞机机翼前梁布局优化进行了研究。

5·The aircraft wing is a continuous structure which goes through the fuselage between Frames 36 and 42.

飞机机翼是一个连续的结构体，通过机身隔框36和42之间。

6·Making aircraft wing vary under different flying speeds is a key technology of variable camber adaptive wing.

实现机翼在不同的飞行状态下的最优气动外形是变弯度自适应机翼的一项关键技术。

7·Ensuring the stability of the composite skin is of great significance in the design of aircraft wing structures.

复合材料蒙皮稳定性是飞机翼面结构设计需要考虑的重要方面。

8·Teeth replaced with ceramics17 as strong as a suborbital18 aircraft wing, and as white as the dorm's good China?

还是说她的牙齿全部都要换成和航天飞机机翼一样坚固、和宿舍里的精致瓷器一般洁白的烤瓷牙？

9·Teeth replaced with ceramics17 as strong as a suborbital18 aircraft wing, and as white as the dorm's good China?

还是说她的牙齿全部都要换成和航天飞机机翼一样坚固、和宿舍里的精致瓷器一般洁白的烤瓷牙？ ？

10·A method for reworking an aircraft wing, attached to an aircraft fuselage, to reduce a propensity for advanced dynamic changes is described.

描述了一种用于再加工飞行器机翼以便减少复杂动力学变化的倾向的方法，其中所述飞行器机翼连接到飞行器机身。