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含预制脱粘的加筋壁板损伤扩展 被引量:3

DAMAGE EXPANSION OF STIFFENED PANEL WITH PREFABRICATED DEBONDING
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摘要 复合材料加筋壁板在制备过程中容易在筋条蒙皮胶界面处存在缺陷,加速了蒙皮与筋条界面脱粘,在极大程度上影响结构的承载能力。基于Abaqus有限元软件用内聚力模型(CZM)和虚拟裂纹闭合技术(VCCT)两种方法对筋条蒙皮界面含预制脱粘的加筋壁板损伤扩展进行研究,并对比试验结果验证了模型的合理性。给出预制脱粘前缘损伤起始时各型能量释放率的分布;进一步研究不同预制脱粘的位置、面积对加筋板最终破坏状态和结构承载能力的大小。对比发现脱粘前缘损伤起始时II型能量释放率的贡献最大;预制脱粘位于外侧时结构的承载能力比位于中部强;结构的承载能力随着预制脱粘面积的增加而减小。 Composite stiffened panels always have defects at the bonding surface in preparation,which accelerates the debonding of the interface between skin and stringer,greatly affects the bearing capacity of the structure.The model of stiffened panel with prefabricated debonding at the interface of stiffened strip and skin was established with both cohesive zone model(CZM)and virtual crack closure technique(VCCT)in ABAQUS,and the rationality of model was verified by experiments.The distribution of energy release rate in prefabricated debonding leading edge was given and the effect of debonding position and area on stiffness and carrying capacity was analyzed.The results indicate that the contribution of type II energy release rate to damage initiation is the greatest;the bearing capacity of the prefabricated debonding structure is stronger than that is in the middle when it is located in outside;the carrying capacity of the structure decrease with the increase of prefabricated debonding area.
作者 张茹 柴亚南 张阿盈 陈向明 ZHANG Ru;CHAI YaNan;ZHANG Aying;CHEN XiangMing(Aircraft Strength Research Institute of China,AVIC,Xi9 an 710065,China)
出处 《机械强度》 CAS CSCD 北大核心 2020年第3期716-722,共7页 Journal of Mechanical Strength
关键词 内聚力模型 虚拟裂纹闭合技术 能量释放率 脱粘 刚度 Cohesive zone model Virtual crack closure technique Energy release rate Debonding Stiffness
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  • 1解德,钱勤,李长安.断裂力学中的数值计算方法及工程应用[M].北京:科学出版社,2009.18-20.
  • 2Christensen R M. Tensor transformation and failure criteria for analy- sis of fiber composite materials. Journal of Composite materials, 1988 ; 22 (9) :874--898.
  • 3Jones R. Studies in the matrix dominated failures of composite joints. Composite Structures, 1999 ;44 ( 1 ) :745--748.
  • 4Kim J S, Oh Jinho. Efficient analysis of laminated composite and sandwhich plates with interfacial imperfectiongs. Composite, 2011 ;42 (2) :1066--1075.
  • 5Cuntze R G. The predictive capability of failure mode concept-based strength criteria for multi-directional laminates. Composites Science and Technology, 2003 ;64:487--516.
  • 6Knops M. Analysis of failure in fiber polymer laminates. Germany: 12008 Springer-Verlag Berlin Heidelberg New York, 2008 : 118--133.
  • 7陈向明.粘接元接触技术在复合材料连接分析中的应用.西安.中国飞机强度研究所,2011:24-26.
  • 8ABAQUS/Standard version 6.9. User's Manual, Hibbit, Karlsson and Sorensen Inc. , Rhode Island, USA, 1998.
  • 9陈绍杰 等.复合材料设计手册[M].北京:航空工业出版社,1990..
  • 10铁摩辛柯SP,盖莱JM.弹性稳定理论[M]. 2版.北京:科学出版社,1965: 418-457.

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