Compressive failure of fiber composites under multi-axial loading

被引:60
作者
Basu, S [1 ]
Waas, AM [1 ]
Ambur, DR [1 ]
机构
[1] Univ Michigan, Dept Aerosp Engn, Composite Struct Lab, Ann Arbor, MI 48109 USA
基金
美国国家航空航天局;
关键词
fiber kinking; compressive failure; multiaxial loading;
D O I
10.1016/j.jmps.2005.09.004
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
This paper examines the compressive strength of a fiber reinforced lamina under multi-axial stress states. An equilibrium analysis is carried out in which a kinked band of rotated fibers, described by two angles, is sandwiched between two regions in which the fibers are nominally straight. Proportional multi-axial stress states are examined. The analysis includes the possibility of bifurcation from the current equilibrium state. The compressive strength of the lamina is contingent upon either attaining a load maximum in the equilibrium response or satisfaction of a bifurcation condition, whichever occurs first. The results show that for uniaxial loading a non-zero kink band angle # produces the minimum limit load. For multi-axial loading, different proportional loading paths show regimes of bifurcation dominated and limit load dominated behavior. The present results are able to capture the beneficial effect of transverse compression in raising the composite compressive strength as observed in experiments. (c) 2005 Elsevier Ltd. All rights reserved.
引用
收藏
页码:611 / 634
页数:24
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