A new mixed mode test for carbon/epoxy composite systems

被引:23
作者
Tracy, GD
Feraboli, P [1 ]
Kedward, KT
机构
[1] Univ Calif Santa Barbara, Dept Mech Engn, Santa Barbara, CA 93106 USA
[2] Raytheon Infrared Operat, Goleta, CA 93107 USA
基金
美国国家航空航天局;
关键词
mixed mode delamination; fracture toughness;
D O I
10.1016/S1359-835X(03)00205-7
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The present research examines analytically and experimentally the mixed mode interlaminar fracture toughness of a resin film infused (RFI) carbon fiber/epoxy laminate, namely a IM7-AS4/3501-6 hybrid composite system. The inability to develop representative interlaminar failure in composites with current mixed mode test configurations motivated this particular investigation. The paper is part of a more extensive research effort concerned with the effects of stitching upon the mixed mode fracture toughness of a RFI composite. A new mixed mode test configuration is suggested, the Single Leg Four Point Bend (SLFPB), which provides a robust method with small specimens and a simple apparatus. Closed form fracture mechanics-based strain energy release (SERR) calculations have been established for this configuration. Finite element analysis was conducted to validate the closed form solution. Results show a very good agreement between analytical solutions, numerical simulation and the newly designed SLFPB experimental test. (C) 2003 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1125 / 1131
页数:7
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