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制备了帽型、泡型、工字型三种夹芯结构复合材料,研究三种夹芯结构在弯曲载荷下的响应行为,并利用有限元的方法研究夹芯结构在弯曲载荷下Von-Mises应力分布,利用Tsai-Hill屈服准则判定有限元模型的屈服情况,观察发生屈服的区域.结果表明,帽型夹芯结构具有最大的弯曲刚度与抗弯强度.三种夹芯结构发生破坏的区域不同,帽型夹芯结构破坏主要出现在压头区域、上面板的压头边缘区域、芯子压头正下方的拐角处;泡型夹芯结构破坏出现在芯子支撑区域;工字型夹芯结构破坏出现在下面板支撑区域.

参考文献

[1] 李晓宇;王佩艳;李祚军;谯盛军.碳纤维/PMI泡沫夹芯复合材料的弯曲特性分析[J].科学技术与工程,2013(5):1261-1265.
[2] 陈启军 .复合材料飞轮转子的失效分析与强度预测[D].郑州大学,2014.
[3] Zhibin Li;Zhijun Zheng;Jilin Yu;Chunqiang Qian;Fangyun Lu.Deformation and failure mechanisms of sandwich beams under three-point bending at elevated temperatures[J].Composite structures,2014May(May):285-290.
[4] 张志峰 .先进复合材料格栅加筋结构优化设计与损伤分析[D].大连理工大学,2008.
[5] 刘勇;陈世健;高鑫;康兴无.基于Hashin准则的单层板渐进失效分析[J].装备环境工程,2010(1):34-39.
[6] Jin Zhang;Peter Supernak;Simon Mueller-Alander;Chun H. Wang.Improving the bending strength and energy absorption of corrugated sandwich composite structure[J].Materials & design,2013Dec.(Dec.):767-773.
[7] Peiyan Wang;Yin Lei;Zhufeng Yue.Experimental and numerical evaluation of the flexural properties of stitched foam core sandwich structure[J].Composite structures,2013Jun.(Jun.):243-248.
[8] Machining FEM model of long fiber composites for aeronautical components[J].Composite structures,20103(3):691.
[9] Chun Lu;Ping Chen;Qi Yu.Thermal Residual Stress Distribution in Carbon Fiber/Novel Thermal Plastic Composite[J].Applied composite materials,20083(3):157-169.
[10] Jian Xiong;Li Ma;Ariel Stocchi;Jinshui Yang;Linzhi Wu;Shidong Pan.Bending response of carbon fiber composite sandwich beams with three dimensional honeycomb cores[J].Composite structures,2014Feb.(Feb.):234-242.
[11] Gefu Ji;Zhenyu Ouyang;Guoqiang Li.Debonding and impact tolerant sandwich panel with hybrid foam core[J].Composite structures,2013Sep.(Sep.):143-150.
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