INTERFACE DEBONDING IN FATIGUE CYCLING OF GLASS REINFORCED-PLASTICS

被引:8
作者
HORSTEMEYER, MF
STAAB, GH
机构
[1] Sandia National Laboratory, Livermore
[2] The Ohio State University, Columbus
关键词
failure; fatigue; fiber breakage; interface debond ing; matrix cracking; strain; strain energy density; Young's modulus;
D O I
10.1177/073168449000900502
中图分类号
TB33 [复合材料];
学科分类号
摘要
The fatigue failure mechanisms of three unidirectional laminated compos ite material systems (consisting of a common fiber in varying resin matrices) were investi gated. Static tensions tests of the pure resins and composites in the axial direction were analyzed in conjunction with fatigue test data to determine failure characteristics. The resins with the highest strain energy density and ultimate strain exhibited the best fatigue properties. A comparison of fatigue curves for both pure resins and composites data showed that the dominant failure mechanism in fatigue is a combination of matrix cracking and interface debonding. © 1990, SAGE PUBLICATIONS. All rights reserved.
引用
收藏
页码:446 / 455
页数:10
相关论文
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