Nonlinear modeling of delaminated struts

被引:31
作者
Hunt, GW [1 ]
Hu, B [1 ]
Butler, R [1 ]
Almond, DP [1 ]
Wright, JE [1 ]
机构
[1] Univ Bath, Dept Mech Engn, Bath BA2 7AY, Avon, England
关键词
D O I
10.2514/1.5981
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
A phenomenological overview of the buckling and postbuckling of fully and partially delaminated struts is developed using a simple four-degree-of-freedom nonlinear Rayleigh-Ritz formulation. Bifurcation analysis indicates that instability occurs in general at an asymmetric point of bifurcation. After bifurcation, realistic solutions are seen to follow the stable part of the postbuckling path, with the unstable branch being denied by contact between the contributing laminates. Depending on the geometry and position of the delamination, thoroughly stable (thin-film), effectively neutral (overall), or potentially unstable (mixed-mode) buckling can occur in the postbuckling range. Numerically obtained equilibrium solutions of the model are found to compare well with those obtained using the finite element code ABAQUS. Critical delamination depths, where the response undergoes a change in form, are discovered at positions of secondary bifurcation. The multiplicity of equilibrium solutions that arise at such points are seen to cause possible problems of path selection for standard finite element routines.
引用
收藏
页码:2364 / 2372
页数:9
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