Bucking and vibration analysis of composite plate and shell structures using the PASSAS software package

被引:13
作者
Dawe, DJ [1 ]
Wang, S
机构
[1] Univ Birmingham, Sch Civil Engn, Birmingham B15 2TT, W Midlands, England
[2] Univ Loughborough, Dept Aeronaut & Automot Engn & Transport Studies, Loughborough LE11 3TU, Leics, England
关键词
D O I
10.1016/S0263-8223(97)00090-1
中图分类号
O3 [力学];
学科分类号
08 ; 0801 ;
摘要
A description is given of the PASSAS finite strip software package for predicting the buckling stresses and natural frequencies of composite laminated prismatic plate and shell structures of complicated cross-section and general lamination. The basic equations underpinning the development of the properties of a transversely curved finite strip are presented in the context of first-order shear-deformation shell theory and, by reduction, in the context of thin shell theory. The B-spline finite strip method is used and this enables the specification of a wide range of end conditions. The major features of the software package are described, and these include a range of strip models, the use of multi-level substructuring techniques across the structure, including superstrips, and the use of an efficient and reliable solution procedure. Results are presented of the application of PASSAS to the solution of a small number of shell buckling and vibration problems. (C) 1997 Elsevier Science Ltd.
引用
收藏
页码:541 / 551
页数:11
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