Bolted double-lap composite joints under mechanical and thermal loading

被引:27
作者
Kradinov, V
Barut, A
Madenci, E
Ambur, DR
机构
[1] Univ Arizona, Dept Aerosp & Mech Engn, Tucson, AZ 85721 USA
[2] NASA, Langley Res Ctr, Mech & Durabil Branch, Hampton, VA 23665 USA
关键词
bolt; double lap; joint; composite; mechanical; thermal;
D O I
10.1016/S0020-7683(01)00128-7
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
This study concerns the determination of the contact stresses and contact region around bolt holes and the bolt load distribution in single- and double-lap joints of composite laminates with arbitrarily located bolts under general mechanical loading conditions and uniform temperature change. The unknown contact stress distribution and contact region between the bolt and laminates and the interaction among the bolts require the bolt load distribution, as well as the contact stresses, to be as part of the solution. The present method is based on the complex potential theory and the variational formulation in order to account for bolt stiffness, bolt-hole clearance, and finite geometry of the composite laminates. (C) 2001 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:7801 / 7837
页数:37
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