1·His suggestion led directly to the creation of the Chinese American Composite Wing.
他的意见直接导致了中美空军混合编队的成立。
2·In this paper, an effective design optimization method for High-aspect-ratio composite wing skin is presented.
论文以大展弦比飞翼布局机翼蒙皮的优化设计为背景，开展了复合材料层压板结构的优化设计工作。
3·The composite wing wall with staggered rigid wing wall and reinforced earth has fulfilled the requirement of stability against sliding and seepage.
采用刚性翼墙与加筋土间隔、上下错开的布置型式，形成复合式翼墙结构，满足挡墙的抗滑稳定性及防渗要求。
4·Composite wing design, in which involved are many disciplines such as structural mechanics, aerodynamics and control engineering, is a complicated process.
复合材料翼面设计是一个涉及结构力学、空气动力学和控制工程等多个学科的复杂过程。
5·To increase the whole strength and stiffness of the composite wing and to lower the manufacturing cost, the main component of the wing is employed with stitched technique.
为了提高复合材料机翼的整体强度和刚度，降低制造成本，机翼的主要结构件采用缝编技术。
6·HDO divides the integrated optimization of composite wing structures into two sub-problems that are easy to be solved: upper level optimization and lower level optimization.
它将复合材料翼面结构综合优化设计问题分解成两个易于求解的子问题：顶层优化设计和底层优化设计。
7·Two types of lay-ups of the composite wing, namely, circumferentially uniform stiffness (CUS) configuration and circumferentially asymmetric stiffness (CAS) configuration, are investigated.
研究了机翼的两种铺设方式：即周向均匀刚度配置（CUS）和周向反对称刚度配置（CAS）。
8·Abstract :Failure process of a primary load-bearing composite joint in wing root was analyzed by finite element methods, and the ultimate strength of the joint was predicted.
以复合材料机翼翼根后梁下缘条对接试件为研究对象，通过有限元手段分析其失效机理和破坏过程，并对极限强度进行预测。
9·It is of great significance and difficulty to ensure the stability of the composite corrugated panels in the design of aircraft wing structures.
复合材料波纹板稳定性是飞机机翼结构设计需要考虑的重要方面，是目前飞机结构设计中的一大难点。
10·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。