Progressive delamination using interface elements

被引:507
作者
Mi, Y
Crisfield, MA
Davies, GAO
Hellweg, HB
机构
[1] Univ London Imperial Coll Sci Technol & Med, Dept Aeronaut, London SW7 2BY, England
[2] Continental AG, Tyre Res, D-30001 Hannover, Germany
关键词
D O I
10.1177/002199839803201401
中图分类号
TB33 [复合材料];
学科分类号
摘要
The paper describes a method for modelling progressive mixed-mode delamination in fibre composites. The procedure, which is incorporated within the non-linear finite element method, is based on the use of interface elements in conjunction with softening relationships between the stresses and the relative displacements. Fracture mechanics is indirectly introduced by relating the areas under the stress/displacement curves to the critical fracture energies.
引用
收藏
页码:1246 / 1272
页数:27
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