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| 非对称非均衡层板弯扭耦合效应研究 | |
| 引用本文： | 许德伟,郦正能,崔德刚.非对称非均衡层板弯扭耦合效应研究[J].北京航空航天大学学报,2001,27(2):167-170. |
| 作者姓名： | 许德伟 郦正能 崔德刚 |
| 作者单位： | 1. 北京航空航天大学 飞行器设计与应用力学系; 2. 航空工业总公司 科技局 |
| 基金项目： | 国家自然科学基金;59675036; |
| 摘 要： | 在对称层板的基础上添加铺层使得整个层板成为非对称或非均衡层板,用数值计算方法对添加铺层后的层板在拉或弯载荷下由于弯扭耦合效应产生的端面变形进行了研究,得到了最有利的添加层铺层位置和添加层铺设角,并用蜂窝夹芯板模拟机翼翼盒进行了实验验证.实验表明,从数值计算所得到的结果与实验结果相比具有良好的一致性. |
| 关 键 词： | 耦合 复合材料 层板 非对称非均衡层板 扭转变形 |
| 文章编号： | 1001-5965(2001)02-0167-04 |
| 收稿时间： | 1999-10-18 |
| 修稿时间： | 1999年10月18日 |
Bend/Twist Coupling Effects of Unsymmetric and Unbalanced Laminate |
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| XU De-wei,LI Zheng-neng,CUI De-Gang.Bend/Twist Coupling Effects of Unsymmetric and Unbalanced Laminate[J].Journal of Beijing University of Aeronautics and Astronautics,2001,27(2):167-170. | |
| Authors: | XU De-wei LI Zheng-neng CUI De-Gang |
| Institution: | 1. Beijing University of Aeronautics and Astronautics, Dept. of Flight Vehicle Design and Applied Mechanics; 2. Science and Technology Bureau of AVIC |
| Abstract: | In order to obtain particular twist angle of composite structure, utilizing the coupling effects of unsymmetric&unbalanced laminate is a considerable approach. An unsymmetric&unbalanced laminate is formed by adding a sub laminate into the symmetric laminate. How to lay the sub laminate and what the optimal orientation angle of the sub laminate is are studied in order to make the most use of coupling effects by nonlinear finite element methods. Test results of honeycomb core sandwich composite laminate simulating the wing box under the load of aerodynamics demonstrate that the calculating results well accord with the test results and unsymmetric&unbalanced laminates have prospective engineering applications. |
| Keywords: | coupling composite materials laminates unsymmetric and unbalanced laminate twisting distortion |
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