考察了复合材料蒙皮与筋条铆接问题。
The problems of riveting of composite face plates are studied.
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。
Ensuring the stability of the composite skin is of great significance in the design of aircraft wing structures.
不同性质缺陷的最佳检测时间不同，对于铝蜂窝铝蒙皮结构复合材料蒙皮的各种脱粘缺陷，检测速度都高于每分钟两屏。
The optimal testing time for different defects is different, and the testing speed is higher than two screens per minute for all bonding defects of honey…
本文采用落锤冲击试验机对铝蒙皮整体中空夹层复合材料进行了低速冲击试验。
This paper presents experimental investigations on low-velocity impact response of hollow integrated sandwich composites with aluminum skin by using drop-weight method.
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。
In this paper, an effective design optimization method for High-aspect-ratio composite wing skin is presented.
采用有限元数值模拟方法，研究了蒙皮内含分层损伤复合材料格栅加筋板结构(ags)的稳定性问题。
A finite element method was developed for the numerical analysis of advanced grid stiffened structure (AGS), and the stability problem of AGS with an embedded delamination was investigated.
采用有限元数值模拟方法，研究了蒙皮内含分层损伤复合材料格栅加筋板结构(ags)的稳定性问题。
A finite element method was developed for the numerical analysis of advanced grid stiffened structure (AGS), and the stability problem of AGS with an embedded delamination was investigated.
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