通过对机翼上壁板半圆切单接头长桁端头试验件进行轴向压缩测试,测得了整个试验件的载荷-应变曲线.试验结果表明,破坏主要集中在接头与长桁缘条连接区域第一排螺钉所对应的复合材料结构压溃断裂,与接头相连的长桁缘条发生长纤维断裂.建立了相应的有限元模型,因为有限元计算中未考虑损伤及刚度衰减,导致有限元分析结果比实际的试验结果略高.
参考文献
[1] | 李玮;段成红;吴祥.碳纤维复合材料强度的有限元模拟[J].玻璃钢1复合材料,2011(1):20-23. |
[2] | 李成;郑艳萍.机械连接结构中含圆孔复合材料板的应力计算及仿真分析[J].玻璃钢/复合材料,2007(3):3-5,51. |
[3] | 张承学,魏兵,惠战荣,蔡新锁.复合材料单筋长桁端头低能量冲击试验研究[C].第七届全国MTS材料试验学术会议论文集,2007:248-251. |
[4] | 张俊鼎;陈斌.复合材料机翼上壁板剖面形状选择研究[J].科技信息,2013(12):445-447. |
[5] | Hollmann K..FAILURE ANALYSIS OF BOLTED COMPOSITE JOINTS EXHIBITING IN-PLANE FAILURE MODES[J].Journal of Composite Materials,19963(3):358-383. |
[6] | A.C. Orifici;R.S. Thomson;I. Herszberg;T. Weller;R. Degenhardt;J. Bayandor.An analysis methodology for failure in postbuckling skin-stiffener interfaces[J].Composite structures,20081/3(1/3):186-193. |
[7] | Shokrieh MM.;Lessard LB..EFFECTS OF MATERIAL NONLINEARITY ON THE THREE-DIMENSIONAL STRESS STATE OF PIN-LOADED COMPOSITE LAMINATES[J].Journal of Composite Materials,19967(7):839-861. |
[8] | K.I. Tserpes;G. Labeas;P. Papanikos;Th. Kermanidis.Strength prediction of bolted joints in graphite/epoxy composite laminates[J].Composites, Part B. Engineering,20027(7):521-529. |
[9] | Falzon BG.;Davies GAO..The Behavior of compressively loaded stiffener runout specimens - Part I: Experiments[J].Journal of Composite Materials,20035(5):381-400. |
[10] | S. Psarras;S.T. Pinho;B.G. Falzon.Design of composite stiffener run-outs for damage tolerance[J].Finite elements in analysis & design,20118(8):949-954. |
[11] | S. Psarras;S.T. Pinho;B.G. Falzon.Investigating the use of compliant webs in the damage-tolerant design of stiffener run-outs[J].Composites, Part B. Engineering,20131(1):70-77. |
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