Effect of Stitching on Plain and Open-hole Strength of CFRP Laminates

被引:15
|
作者
Zheng Yun [2 ]
Cheng Xiaoquan [1 ]
Yasir, Baig [1 ]
机构
[1] Beihang Univ, Sch Aeronaut Sci & Engn, Beijing 100191, Peoples R China
[2] Beihang Univ, Sch Econ & Management, Beijing 100191, Peoples R China
基金
中国国家自然科学基金;
关键词
composite materials; stitching; finite element method; resin film infusion; hygrothermal; CARBON-FIBER COMPOSITES; MOISTURE ABSORPTION; BISMALEIMIDE RESIN; EPOXY COMPOSITES; BEHAVIOR; DIFFUSION;
D O I
10.1016/S1000-9361(11)60411-1
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
Experimental and analytical investigation is conducted to explore the effects of stitching on plain (without hole) and open-hole compressive and tensile strength of uniweave T300/QY9512 laminates under different environmental conditions (20 degrees C/dry and wet, 150 degrees C/dry and wet). Strength performance of stitched composite laminates is also studied using finite element analysis (FEA) model and compared with the experimental results to validate the model. It is found that under similar environmental conditions, the open-hole compressive strength of stitched laminate is decreased and open-hole tensile strength increased as compared to the unstitched laminates. Predicted tensile and compressive strengths are found to be in a good agreement with the test results and the relative error in all cases is less than 15%.
引用
收藏
页码:473 / 484
页数:12
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