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复合材料整体加筋板轴压后屈曲失效表征
引用本文:孔斌,叶强,陈普会,柴亚南.复合材料整体加筋板轴压后屈曲失效表征[J].复合材料学报,2010,27(5):150-155.
作者姓名:孔斌  叶强  陈普会  柴亚南
作者单位:1. 南京航空航天大学,航空宇航学院,南京,210016
2. 中国飞机强度研究所,西安,710065
基金项目:国家自然科学基金(10872091)
摘    要:应用商业有限元软件ABAQUS中的内聚单元,对后屈曲诱发的复合材料整体加筋板的缘条/蒙皮界面的失效进行了分析。基于有限元结果,提出了缘条/蒙皮界面内力的提取方法并研究了其变化规律。为了研究缘条/蒙皮刚度比对界面失效的影响以及失效时界面内力之间的关系,以缘条厚度为参数进行参数化建模,给出了界面脱胶的失效准则和失效包线。最后对缘条/蒙皮厚度比和刚度比提出了设计建议。

关 键 词:复合材料  整体加筋板  后屈曲  内聚单元    失效表征
收稿时间:2009-09-29
修稿时间:2009-12-21

Post-buckling failure characterization of an integrated stiffened composite panel under uniaxial compression
KONG Bin,YE Qiang,CHEN Yuhui,CHAI Ya'nan.Post-buckling failure characterization of an integrated stiffened composite panel under uniaxial compression[J].Acta Materiae Compositae Sinica,2010,27(5):150-155.
Authors:KONG Bin  YE Qiang  CHEN Yuhui  CHAI Ya'nan
Affiliation:KONG Bin1,YE Qiang1,CHEN Puhui1,CHAI Ya'nan2(1.School of Aerospace Engineering,Nanjing University of Aeronautics and Astronautics,Nanjing 210016,China,2.Aircraft Strength Research Institute,Xi'an 710065,China)
Abstract:The post-buckling induced failure process was simulated by using the cohesive element in the commercial software ABAQUS. The internal forces on the flange/skin interface were extracted from FEM results, and then their features were studied. The flange thickness was considered as a parameter to build a parameterized model for studying the effect of stiffness ratios of the flange to the skin on the interface debonding. The relationship among each component of the internal forces was also investigated. Failure criteria and failure envelops were developed for the flange/skin interface debonding. Finally the design parameters of the thickness ratio and the stiffness ratio between the flange and the skin were suggested for the design.
Keywords:composite  integrated stiffened panel  post-buckling  cohesive element  failure characterization
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