On the feasibility of using thermal gradients for active control of interlaminar stresses in laminated composites

被引:13
作者
Kim, T [1 ]
Steadman, D [1 ]
Hanagud, SV [1 ]
Atluri, SN [1 ]
机构
[1] GEORGIA INST TECHNOL,FAA,CTR EXCELLENCE COMPUTAT MODELING AIRCRAFT STRUCT,ATLANTA,GA 30332
关键词
D O I
10.1177/002199839703101601
中图分类号
TB33 [复合材料];
学科分类号
摘要
In this paper, a method is proposed to actively control interlaminar stresses near the free edges of laminated composites by through-thickness thermal gradients. Theoretical solutions are given for optimal steady-state through-thickness temperature distributions under uniaxial loading that are required to elmininate or reduce the interlaminar stresses below a prescribed level. The optimal solutions are obtained by minimizing appropriate performance indices that are functions of the far-field properties, with respect to the through-thickness temperature differences. In the second part, an experimental investigation is conducted on a glass/epoxy cross-ply laminate with embedded piezoelectric sensors and a thermal heater. Through the experiment, the feasiblity of the thermal control of interlaminar stresses is demonstrated.
引用
收藏
页码:1556 / 1573
页数:18
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