首页 | 本学科首页   官方微博 | 高级检索  
     检索      

复合材料层板等强最优设计方法
引用本文:刘方龙,黄季墀.复合材料层板等强最优设计方法[J].航空学报,1984,5(2):200-209.
作者姓名:刘方龙  黄季墀
作者单位:北京航空学院 (刘方龙),北京航空学院(黄季墀)
摘    要: 本文对复合材料无矩对称层板的最优设计,提出了一种概念直观、方法简便、收敛迅速、效果较好的等强最优设计方法。给出了几个算例的结果,并与文献1、2]的方法作了对比,结果表明,本文的方法具有显著的优越性。

关 键 词:
收稿时间:1982-11-01;

AN EQUIVALENT STRENGTH METHOD FOR OPTIMUM DESIGN OF COMPOSITE LAMINATES
Liu Fanglong.AN EQUIVALENT STRENGTH METHOD FOR OPTIMUM DESIGN OF COMPOSITE LAMINATES[J].Acta Aeronautica et Astronautica Sinica,1984,5(2):200-209.
Authors:Liu Fanglong
Institution:Beijing Institute of Aeronautics and Astronautics
Abstract:An equivalent strength method for optimum design , of composite laminated plates subjected to an in-plane arbitrary loading is presented as an intuitive and simple engineering method. The method affirms that the design of composite laminate is optimum when the strength ratios of each lamina are epuivalent and equal to one. This is a criterion. It can be considered that the orientations of individual ply groups are determined, but the thickness of each group can be adjusted in accordance with the principle of the equivalent strength ratio, in result the failure of statical tension,compression or shear in each ply of laminate under the designed loads happens at the same time. In design optimization by the equivalent strength method the thickness and the weight of a laminated plate are minimized. Five numerical examples are given and compared with corresponding data in references1]and2]. The results show that the equivalent strength method is better than the methods employed in references1]and2].
Keywords:
本文献已被 CNKI 等数据库收录!
点击此处可从《航空学报》浏览原始摘要信息
点击此处可从《航空学报》下载免费的PDF全文
设为首页 | 免责声明 | 关于勤云 | 加入收藏

Copyright©北京勤云科技发展有限公司  京ICP备09084417号