QQ客服 官方微博 反馈留言

	Optimum in situ strength design of laminates under combined mechanical and thermal loads
	Wang, J ; Karihaloo, BL
	1999
关键词	in situ strength optimum design thermal load failure criterion first-ply-failure LAYER THICKNESS COMPOSITES GRAPHITE FAILURE ANGLE
英文摘要	In this paper, optimum laminate configurations are sought for multidirectional fibre-reinforced composite laminates under combined in-plane mechanical and thermal loads. The design objective is to enhance the value of the loads over and above the first-ply-failure loads which are judged by a transverse failure criterion and the Tsai-Hill criterion, respectively. The in situ strength parameters previously obtained are incorporated in these criteria. It is found that the optimum designs under combined mechanical and thermal loads are not the same as those under pure mechanical loads for three of the four loading cases studied. For ail cases the optimum loads are significantly larger than those for a quasi-isotropic design. (C) 2000 Elsevier Science Ltd. All rights reserved.; http://gateway.webofknowledge.com/gateway/Gateway.cgi?GWVersion=2&SrcApp=PARTNER_APP&SrcAuth=LinksAMR&KeyUT=WOS:000089300500026&DestLinkType=FullRecord&DestApp=ALL_WOS&UsrCustomerID=8e1609b174ce4e31116a60747a720701 ; Materials Science, Composites; SCI(E); EI; CPCI-S(ISTP); 12
语种	英语
DOI标识	10.1016/S0263-8223(00)00040-4
内容类型	其他
源URL	[http://ir.pku.edu.cn/handle/20.500.11897/154157]
专题	工学院
推荐引用方式 GB/T 7714	Wang, J,Karihaloo, BL. Optimum in situ strength design of laminates under combined mechanical and thermal loads. 1999-01-01.

个性服务

查看访问统计

相关权益政策

暂无数据

收藏/分享

除非特别说明，本系统中所有内容都受版权保护，并保留所有权利。