缝合复合材料T型接头拉伸载荷下的有限元数值模拟

doi:10.7527/S1000-6893.2020.24231

Abstract

Abstract: Software ABAQUS is used to model and analyze the stitched T-joint under tensile load. The cohesive contact method based on the Cohesive Zone Model (CZM) is adopted to simulate the debonding behavior of the stiffener flange and skin. The reinforcement effect of stitching at the interface is simulated with the nonlinear spring element based on mesomechanics. On the basis of finite element model, the influence of stitching on tensile properties of the T-joint is studied by parametric analysis. Results show that the ultimate failure load increases with the increase of the thread diameter. That is, the tensile bearing capacity improves. The analysis results of the finite element method are in good agreement with the experimental values. It is worth noting that there is a 10.4% deviation between the simulation results and the experimental values when the thread diameter increases to 1 500 denier, because the model does not consider the effect of stitching on the in-plane performance and ignores the possible damage caused by stitching. Since the failure modes of the T-joint under tensile load are mainly Type I and Type Ⅱ failures, it is advisable to use two-dimensional finite element model for parametric analysis for its high calculation efficiency and good agreement with the test results.

Key words: finite element, stitching, composites, T-joint, tensile load

CLC Number:

V258
TB332

WEN Liwei, YU Kun, HUAN Huasong. Finite element numerical simulation of stitched composite T-joint under tensile load[J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2021, 42(2): 224231-224231.

References

[1] 李陵, 徐峰, 郑绍文. 复合材料T型接头力学性能分析及优化研究[J]. 玻璃钢/复合材料, 2015(4):41-46. LI L, XU F, ZHENG S W. Research and analysis on the mechanical properties and optimization for composite T-joint[J]. Fiber Reinforced Plastics/Composites, 2015(4):41-46(in Chinese).
[2] BORTOLUZZI D B, GOMES G F, HIRAYAMA D, et al. Development of a 3D reinforcement by tufting in carbon fiber/epoxy composites[J]. The International Journal of Advanced Manufacturing Technology, 2019,100(5/8):1593-1605.
[3] BIGAUD J, ABOURA Z, MARTINS A T, et al. Analysis of the mechanical behavior of composite T-joints reinforced by one side stitching[J]. Composite Structures, 2018, 184:249-255.
[4] 程小全, 赵龙, 张怡宁. 缝合复合材料可用性——简单层合板的基本性能[J]. 北京航空航天大学学报, 2003,29(11):1001-1005. CHENG X Q, ZHAO L, ZHANG Y N. Properties of stitched composite laminates——the principle properties of simple laminates[J]. Journal of Beijing University of Aeronautics and Astronautics, 2003,29(11):1001-1005(in Chinese).
[5] 燕瑛, 韩凤宇, 杨东升, 等. 缝合复合材料弹性性能的三维有限元细观分析与试验验证[J]. 航空学报, 2004,25(3):267-269. YAN Y, HAN F Y, YANG D S, et al. Finite element micromechanical analysis and experimental confirmation of the elastic properties of stitched composite materials[J]. Acta Aeronautica et Astronautica Sinica, 2004,25(3):267-269(in Chinese).
[6] MIGNERY L A, TAN T M, SUN C T. The use of stitching to suppress delamination in laminated composites[C]//ASTM STP. West Conshohocken:ASTM International, 1985:371-385.
[7] VELMURUGAN R, SOLAIMURUGAN S. Influence of in-plane fibre orientation on mode I interlaminar fracture toughness of stitched glass/polyester composites[J]. Composites Science and Technology, 2008, 68(7):1742-1752.
[8] 朱华东, 矫桂琼, 杨宝宁. 缝合复合材料Ⅱ型层间断裂韧性研究[J]. 复合材料学报, 2001, 18(2):85-89. ZHU H D, JIAO G Q, YANG B N. Investigation into the effect of stitching in CFRP on mode Ⅱ delamination toughness[J]. Acta Materiae Compositae Sinica, 2001, 18(2):85-89(in Chinese).
[9] 张国利, 李嘉禄, 李学明. T型壁板RFI缝合复合材料的屈曲性能[J]. 纺织学报, 2006(3):67-70. ZHANG G L, LI J L, LI X M. Buckling performance of T-shape RFI stitched composites panel[J]. Journal of Textile Research, 2006(3):67-70(in Chinese).
[10] KIM C H, JO D H, CHOI J H. Failure strength of composite T-joints prepared using a new 1-thread stitching process[J]. Composites Structures, 2017,178:225-231.
[11] 叶强, 陈普会. 复合材料粘聚区模型的强度参数预测[J]. 固体力学学报, 2012,33(6):566-573. YE Q, CHEN P H. Prediction on the strength parameters of cohesive zone model for simulation composite delamination[J]. Chinese Journal of Solid Mechanics, 2012,33(6):566-573(in Chinese).
[12] 孔斌, 陈普会, 李梦佳, 等. Z-pin/缝合对复合材料T型接头剪切承载能力的影响[J]. 复合材料学报, 2018,35(4):834-842. KONG B, CHEN P H, LI M J, et al. Effect of Z-pin/stitching on the shear carrying capacity of composite T-joints[J]. Acta Materiae Compositae Sinica, 2018,35(4):834-842(in Chinese).
[13] IWAHORI Y, NAKANE K, WATANABE N. DCB test simulation of stitched CFRP laminates using interlaminar tension test results[J]. Composites Science and Technology, 2009,69(14):2315-2322.
[14] 李梦佳, 陈普会, 孔斌, 等. Z-pin参数对复合材料T型接头拉脱承载能力的影响[J]. 复合材料学报, 2015,32(2):571-578. LI M J, CHEN P H, KONG B,et al. Effect of Z-pin parameters on pull-off carrying capacity of composite T-joints[J]. Acta Materiae Compositae Sinica, 2015, 32(2):571-578(in Chinese).
[15] GRASSI M, ZHANG X. Finite element analysis of mode I interlaminar delamination in z-fiber reinforced composite laminates[J]. Composites Science and Technology, 2003, 63(12):1815-1832.
[16] TAN K T, WATANABE N. Impact damage resistance, response, and mechanisms of laminated composites reinforced by through-thickness stitching[J]. International Journal of Damage Mechanics, 2012,21(1):51-80.
[17] 程小全, 邹健, 张纪奎,等. 缝合复合材料可用性——含孔层合板的疲劳性能[J]. 航空学报, 2009, 30(5):867-871. CHENG X Q, ZOU J, ZHANG J K,et al. Properties of stitched composite laminates——fatigue performance of composite laminates with an open-hole[J]. Acta Aeronautica et Astronautica Sinica, 2009, 30(5):867-871(in Chinese).
[18] 尹昌平, 李建伟, 刘钧, 等. 缝合/RTM复合材料层合板的力学性能研究[J]. 材料导报, 2007, 21(11):136-138. YIN C P, LI J W, LIU J, et al. Research on mechanical properties of stitched/RTM composite laminates[J]. Materials Reports, 2007, 21(11):136-138(in Chinese).
[19] 盛仪, 熊克, 卞侃, 等. 拉伸状态下碳纤维复合材料T型接头的断裂行为[J].复合材料学报, 2013,30(6):185-190. SHENG Y, XIONG K, BIAN K. Fracture behavior of carbon fiber T-joints under tensile load[J]. Acta Materiae Compositae Sinica, 2013,30(6):185-190(in Chinese).
[20] TURON A, DÀVILA C G, CAMANHO P P, et al. An engineering solution for mesh size effects in the simulation of delamination using cohesive zone models[J]. Engineering Fracture Mechanics, 2007, 74(10):1665-1682.
[21] BIANCHI F, KOH T M, ZHANG X, et al. Finite element modelling of z-pinned composite T-joints[J]. Composites Science and Technology, 2012, 73:48-56.
[22] HUAN D J, LI Y, TAN Y, et al. On the assessment of the load-bearing capacity of Z-pinned composite T-joint under out-of-plane tension[J]. Journal of Reinforced Plastics and Composites, 2017, 36(22):1639-1650.
[23] LI M J, CHEN P H, LI X P, et al. Experimental and numerical study on the tensile properties of T-joints with low Z-pin volume density[J]. Polymer Composites, 2020, 41(1):258-270.

Finite element numerical simulation of stitched composite T-joint under tensile load

RichHTML

PDF (PC)

Knowledge

Abstract

Cite this article

share this article

References

Related Articles 15

Recommended Articles

Metrics

Comments

[1]	Wenbin JIA, Lei FANG, Gen ZHANG, Jian SHI, Zekan HE, Haijun XUAN. Optimal design of fracture toughness for CNT⁃epoxy composites [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(7): 428971-428971.
[2]	Chunyun ZHANG, Xiongbin CHEN, Jian LIU, Miao CUI. Prediction of thermo⁃physical properties of inorganic⁃organic hybrid phenolic aerogel composites [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(6): 428848-428848.
[3]	Lingcai HUANG. Review of nondestructive testing methods for fiber⁃reinforced polymer composites [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(5): 529697-529697.
[4]	Fangyi SHENG, Guolin YANG, Fantong MENG, Zhigang DONG, Renke KANG. Finite element simulation analysis in helical milling of countersunk hole [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 428690-428690.
[5]	Siji WANG, Yuwei ZHANG, Kaiming HUANG, Biao LYU, Haifeng ZHAO, Hu WANG, Mingfu LIAO. An optimization method for helicopter power turbine rotor system based on improved particle swarm optimization algorithm [J]. Acta Aeronautica et Astronautica Sinica, 2024, 45(1): 228608-228608.
[6]	Yongjie HUANG, Zhangsong NI, Jie PAN. Simulation of electro-impulse de-icing considering ice fracture and interface debonding [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(S2): 729306-729306.
[7]	Hongyue WANG, Bing WANG, Guodong FANG, Songhe MENG. Digital element modelling and analysis of 2.5D woven shallow cross bending composites [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(9): 227478-227478.
[8]	Zhenyu WANG, Jizhen WANG, Jingyi YANG, Pengyuan HE, Chenghao PAN, Lingbo ZHOU, Cheng HE, Huan HE. Dynamics model updating of structures at high temperature based on novel particle swarm optimization algorithm [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(7): 226559-226559.
[9]	Liping LIU, Yuyang QI, Yueguo LIN, Rui BAO, Jianxin XU, Zhenyu FENG, Guanghui QING. Tensile failure of carbon fiber composite material bonded-rivet hybrid repaired structure [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(24): 428676-428676.
[10]	Guoqi ZENG, Zifan NIU, Lili ZHENG, Jie LI, Delin HAO. A real time video image stitching method for UAV based on spherical transformation [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(24): 328364-328364.
[11]	Zhenyu MA, Xiaolong DENG, Xixiang YANG, Bingjie ZHU. Thermal⁃structure coupling characteristics of flexible envelopes for stratospheric airships at float conditions [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(19): 228337-228337.
[12]	Yang SUN, Jian HUANG, Chenchen HAN, Zhenqiang ZHAO, Haili ZHOU, Fangfang SUN, Chao LI, Chao ZHANG, Liquan ZHANG. Comparison of in-plane mechanical properties of 2D and 3D woven composites [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(18): 428267-428267.
[13]	Tianchun ZOU, Yuezhang JU, Yuxi GUAN, Zegang LI, Hongcheng CHEN. Effect of stacking sequence on fatigue behavior of CFRP⁃Al joint [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(18): 428264-428264.
[14]	Jiangbo CHEN, Kai ZENG, Baoying XING, Hongshen ZHANG, Yanfang DING, Xiaocong HE. Aluminum alloy clinch-bonding with hot melt adhesive film and joint failure analysis [J]. Acta Aeronautica et Astronautica Sinica, 2023, 44(14): 428029-428029.
[15]	Chao TANG, Wenjun XIE, Peiyu YUAN, Zonghong XIE. Development and verification of a conformal electrothermal deicing functional structure for leading edge of airfoil [J]. ACTA AERONAUTICAET ASTRONAUTICA SINICA, 2023, 44(12): 427872-427872.