丢层结构复合材料加筋板压缩失效机理研究

doi:10.19936/j.cnki.2096-8000.20220528.011

复合材料科学与工程 ›› 2022, Vol. 0 ›› Issue (5): 78-84.DOI: 10.19936/j.cnki.2096-8000.20220528.011

丢层结构复合材料加筋板压缩失效机理研究

薛晗, 余音^*

上海交通大学航空航天学院航空航天飞行器先进结构与材料试验中心,上海 200240

收稿日期:2021-07-26 出版日期:2022-05-28 发布日期:2022-07-19
通讯作者: 余音(1964-),女,博士,副教授,主要从事复合材料结构分析及近场动力学、结构动力学方面的研究,yuyin@sjtu.edu.cn。
作者简介:薛晗(1995-),男,硕士研究生,研究方向为复合材料结构分析。

Study on the compressive failure mechanism of composite stiffened plate with ply drop-off structure

XUE Han, YU Yin^*

Aerospace Vehicle Advanced Structure and Material Test Center, School of Aeronautics and Astronautics Aerospace, Shanghai Jiao Tong University, Shanghai 200240, China

Received:2021-07-26 Online:2022-05-28 Published:2022-07-19

摘要/Abstract

摘要： 为探究受到轴向压缩载荷时丢层结构对复合材料加筋板承载能力、破坏模式及破坏位置的影响,对丢层结构与常规铺层结构两种铺层方式的帽型长桁加筋板进行轴压试验,并通过Abaqus建立了丢层结构复合材料加筋板有限元模型,采用二维Hashin准则作为复合材料失效判据,与试验结合分析了两种构型复合材料加筋板的失效过程及抗压性能。有限元模型很好地预测了结构的极限载荷、破坏模式及破坏位置,与试验结果吻合较好。结果表明:①采用有限元方法得到的极限载荷与实验较吻合,丢层结构与常规结构破坏载荷误差分别为1.1%与4.7%,说明本文采用的建模方法合理有效,可以为实际工程应用提供指导;②合理的丢层结构对长桁承载能力及破坏模式并不会产生影响,但是会影响试验件破坏的位置。

关键词: 复合材料, 加筋板, 丢层结构, 承载能力, 破坏模式

Abstract: In order to investigate the influence on composite stiffened plate load-bearing capacity, failure mode and failure location of the ply drop-off composite structure under axial compression, experimental studies were carried out for hat-shaped stringers with ordinary and ply drop-off layups. Finite Element (FE) models of composite stiffened plates with the ply drop-off structure were established by using Abaqus. The FE models adopt two-dimensional Hashin failure criterion and analyze the failure process and compressive performance of two types of composite stiffened plates. The FE models accurately predict the ultimate load, failure mode and failure location, which are in good agreement with the experimental results. The present study shows that the ultimate load obtained by the finite element (FE) method is in good agreement with the experiment. The failure load error of ply drop-off composite structure and the conventional structure is 1.1% and 4.7%, respectively, indicating that the modeling method adopted in this paper is reasonable and effective, and can provide guidance for practical engineering applications. Inaddition, it shows that appropriate ply drop-off does not influence the load-bearing capacity and failure mode of composite stiffened plate, but it may change the failure location.

Key words: composite material, stiffened plate, the ply drop-off structure, carrying capacity, failure mode

中图分类号:

TB332

薛晗, 余音. 丢层结构复合材料加筋板压缩失效机理研究[J]. 复合材料科学与工程, 2022, 0(5): 78-84.

XUE Han, YU Yin. Study on the compressive failure mechanism of composite stiffened plate with ply drop-off structure[J]. COMPOSITES SCIENCE AND ENGINEERING, 2022, 0(5): 78-84.

参考文献

[1] 常园园. 面内载荷下复合材料整体加筋板破坏过程分析[D]. 南京: 南京航空航天大学, 2010.
[2] ZHU S, YAN J, CHEN Z, et al. Effect of the stiffener stiffness on the buckling and post-buckling behavior of stiffened composite panels-Experimental investigation[J]. Composite Structures, 2015, 120: 334-345.
[3] BISAGNI C, VESCOVINI R, DAVILA C. Assessment of the damage tolerance of post-buckled hat-stiffened panels using single stringer specimens[C]//51st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference 18th AIAA/ASME/AHS Adaptive Structures Conference 12th. 2010: 2696.
[4] 徐荣章, 关志东, 王仁宇, 等. 不同工艺成型复合材料加筋板轴压破坏机理分析[J]. 北京航空航天大学学报, 2016, 42(5): 1032-1038.
[5] 杨钧超, 柴亚南, 张阿盈. 胶接和共固化成型对复合材料加筋板压缩性能的影响[J]. 工程与试验, 2017, 57(1): 14-18.
[6] ZHAO W, XIE Z, WANG X, et al. Buckling behavior of stiffened composite panels with variable thickness skin under compression[J]. Mechanics of Advanced Materials and Structures, 2019, 26(3): 215-223.
[7] MASOOD S N, GADDIKERI K M, VISWAMURTHY S R. Experimental and finite element numerical studies on the post-buckling behavior of composite stiffened panels[J]. Mechanics of Advanced Materials and Structures, 2019, 1677-1690.
[8] 胡祎乐, 余音, 汪海, 等. 纤维增强复合材料机翼长桁压缩破坏预测方法[J]. 上海交通大学学报, 2012, 46(9): 1471-1475.
[9] 李汝鹏, 陈磊, 刘学术, 等. 基于渐进损伤理论的复合材料开孔拉伸失效分析[J]. 航空材料学报, 2018, 38(5): 138-146.
[10] 王跃全, 童明波, 朱书华. 三维复合材料层合板渐进损伤非线性分析模型[J]. 复合材料学报, 2009, 26(5): 159-166.
[11] 刘魏光, 余音, 汪海. 考虑剪切非线性的复合材料渐进损伤模型[J]. 上海交通大学学报, 2016, 50(2): 194-199, 208.
[12] HASHIN Z. Fatigue failure criteria for unidirectional fiber composites[J]. Journal of Applied Mechanics, 1980, 47(2): 846-852.
[13] YE L. Role of matrix resin in delamination onset and growth in composite laminates[J]. Composites Science & Technology, 1988, 33(4): 257-277.
[14] BLACKLOCK J R, RICHARD R M. Finite element analysis of inelastic structures[J]. Aiaa Journal, 2015, 7(3): 432-438.
[15] MUKHERJEE A, VARUGHESE B. Design guidelines for ply drop-off in laminated composite structures[J]. Composites Part B: Engineering, 2001, 32(2): 153-164.

丢层结构复合材料加筋板压缩失效机理研究

Study on the compressive failure mechanism of composite stiffened plate with ply drop-off structure

PDF (PC)

可视化

摘要/Abstract

引用本文

使用本文

参考文献

相关文章 15

编辑推荐

Metrics

本文评价

[1]	王孟, 刘程, 张玉, 贾航, 乔越, 蹇锡高. 成型温度对CF/PPEK复合材料的缺陷和力学性能影响[J]. 复合材料科学与工程, 2024, 0(3): 5-12.
[2]	史洪源, 任文坚, 党杰, 周鹏. 玻璃纤维增强复合材料超声检测声场的CIVA仿真与试验研究[J]. 复合材料科学与工程, 2024, 0(3): 20-24.
[3]	杨思鑫, 曹忠亮, 顾付伟. 双三角点阵夹芯结构低速冲击下的动态响应与失效机制[J]. 复合材料科学与工程, 2024, 0(3): 25-34.
[4]	张斌, 赵晶, 王世杰. Kagome点阵结构参数对其压缩特性的影响及轻质化设计[J]. 复合材料科学与工程, 2024, 0(3): 35-42.
[5]	王宇轩, 曹东风, 胡海晓, 李书欣. 计及层内和层间的L形层合板失效的数值研究[J]. 复合材料科学与工程, 2024, 0(3): 43-53.
[6]	耿健, 董九志, 梅宝龙, 蒋秀明. 三维四向碳/碳复合材料力学性能预测与试验验证[J]. 复合材料科学与工程, 2024, 0(3): 54-60.
[7]	高坤, 张兆恒, 邢亚娟, 左小彪, 王博尧, 赵泽华. 含磷POSS阻燃乙烯基酯树脂性能研究[J]. 复合材料科学与工程, 2024, 0(3): 61-64.
[8]	郑子君, 乔英, 邵家儒. 基于机器视觉的短纤维复合材料的取向度提取方法[J]. 复合材料科学与工程, 2024, 0(3): 65-72.
[9]	许晓婷, 郝恩全, 邵慧奇, 邵光伟, 毕思伊, 陈南梁, 蒋金华. 三维大隔距机织间隔织物柔性复合材料的服役性能研究[J]. 复合材料科学与工程, 2024, 0(3): 73-78.
[10]	苏桐, 胡果馨, 刘振. 全碳纤维复合材料太阳能无人机机翼结构优化设计[J]. 复合材料科学与工程, 2024, 0(3): 79-83.
[11]	伍强, 赵凯, 刘鹏飞, 张涛涛, 朱德勇. Z形纤维增强复合材料层压板固化变形分析[J]. 复合材料科学与工程, 2024, 0(3): 84-90.
[12]	宋贵宾, 黄光启, 杨胜春. 复合材料层压板胶接挖补修理分析方法及影响因素研究[J]. 复合材料科学与工程, 2024, 0(3): 91-96.
[13]	王耀, 邵丹丹, 雷炳育. 共沉淀析出-热压技术制备高储能性能复合材料薄膜[J]. 复合材料科学与工程, 2024, 0(3): 97-102.
[14]	张仲香, 刘宝锋, 方晨鑫, 陈文光, 顾育慧, 李军向. 沙戈荒环境下风电叶片中复合材料耐高温性能研究[J]. 复合材料科学与工程, 2024, 0(3): 103-107.
[15]	邓忠, 支亚非, 程家林, 杨文. 太阳能无人机机翼复合材料主梁铺层优化[J]. 复合材料科学与工程, 2024, 0(3): 108-112.