Comparison of out-of-plane tensile moduli of CFRP laminates obtained by 3-point bending and direct loading tests

被引:20
作者
Hara, Eiichi [1 ]
Yokozeki, Tomohiro [2 ]
Hatta, Hiroshi [3 ]
Iwahori, Yutaka [1 ]
Ishikawa, Takashi [4 ]
机构
[1] Japan Aerosp Explorat Agcy JAXA, IAT, Advanced Composite Res Ctr, Mitaka, Tokyo 1810015, Japan
[2] Univ Tokyo, Dept Aeronaut & Astronaut, Bunkyo Ku, Tokyo 1138656, Japan
[3] Japan Aerosp Explorat Agcy JAXA, Inst Space & Astronaut Sci, Sagamihara, Kanagawa 2298510, Japan
[4] Nagoya Univ, Dept Aerosp Engn, Chikusa Ku, Nagoya, Aichi 4648603, Japan
关键词
Polymer-matrix composites (PMCs); Mechanical properties; Laminate mechanics; Mechanical testing; COMPOSITES;
D O I
10.1016/j.compositesa.2014.08.003
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The out-of-plane tensile modulus of laminated carbon fiber reinforced plastics (CFRPs) was evaluated through 3-point bending tests using laminated UD-CFRP and quasi-isotropic (QI) CFRP samples with out-of-plane span directions. Direct loading tests of QI-CFRP samples were performed for comparison. It was shown that the bending modulus measured for a UD-CFRP specimen with L/t> 25 is consistent with the tensile modulus if the bending modulus is less than 15 GPa. An analytical description of the out-of-plane modulus of thin QI-CFRP samples was derived by modifying the three-dimensional laminate theory and introducing conditions similar to plane-stress. Subsequently, it was demonstrated that this modified out-of-plane modulus is the lower bound of the apparent bending moduli and that the one predicted by the three-dimensional laminate theory is the upper bound. Finally, it was demonstrated that the 3-point bending test method is more practical than a direct loading test when comparing both methods. (C) 2014 Elsevier Ltd. All rights reserved.
引用
收藏
页码:77 / 85
页数:9
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