CFRP laminate out-of-plane tensile modulus determined by direct loading

被引:16
作者
Hara, Eiichi [1 ,2 ]
Yokozeki, Tomohiro [3 ]
Hatta, Hiroshi [4 ]
Iwahori, Yutaka [5 ]
Ishikawa, Takashi
机构
[1] Japanese Aerosp Technol, Fdn Promot, Mitaka, Tokyo 1810015, Japan
[2] Grad Univ Adv Studies, Dept Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan
[3] Univ Tokyo, Dept Aeronaut & Astronaut, Bunkyo Ku, Tokyo 1138656, Japan
[4] Japan Aerosp Explorat Agcy JAXA, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan
[5] Japan Aerosp Explorat Agcy JAXA, Aerosp Res & Dev Directorate, Mitaka, Tokyo 1810015, Japan
关键词
Polymer-matrix composites (PMCs); Mechanical properties; Finite element analysis (FEA); Mechanical testing;
D O I
10.1016/j.compositesa.2010.06.017
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The purpose of the present study was to establish a measuring procedure for the out-of-plane tensile modulus of CFRP laminates using a direct tensile loading method. Experimental results of out-of-plane tensile tests were compared with numerical predictions. Experimental results showed that the apparent strain of unidirectional (UD-) and quasi-isotropic (QI-) CFRP laminates varies with specimen geometry, gage length, and measuring positions in spite of the uniform tensile strain being loaded to the specimen. This tendency was confirmed to be precisely simulated by finite element analyses. Thus, these results should be taken into consideration in evaluating out-of-plane tensile modulus. The mechanisms underlying these strain variations are discussed, and based on the discussion, guidelines are given for using strain gage output in the determination of out-of-plane tensile modulus of the CFRP laminates. (c) 2010 Elsevier Ltd. All rights reserved.
引用
收藏
页码:1538 / 1544
页数:7
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