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- 2018
变刚度复合材料开孔板拉伸行为数值模拟及试验验证
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Abstract:
纤维曲线铺放是提高复合材料构件力学性能的有效方法之一。本文针对复合材料开孔板铺放轨迹进行了研究,利用B样条曲线插值拟合获取了开孔板最大主应力铺放轨迹,并通过离散网格法建立了变刚度开孔板模型,通过引入Tsai-Wu损伤失效判据以及常刚度退化准则,进行了拉伸失效数值模拟及损伤失效分析,并分别铺放了两组常刚度和变刚度开孔板试验样件,进行了拉伸对比试验。结果表明:数值模拟与实验数据吻合较好,变刚度开孔板相比常刚度开孔板,拉伸强度提升了26.92%,且两者损伤失效演化过程显著不同。 Curvilinear fiber format is one of the effective ways to improve the mechanical properties of composite components.The laying trajectories of open-hole composite laminates were investigated. B-spline interpolation was used to obtain the laying trajectory of open-hole composite laminates with the maximum principal stress. The variable stiffness open-hole composite laminate model was established by discrete grid method.The tensile failure numerical simulation and damage failure analysis were carried out by Tsai-Wu damage failure criterion and constant stiffness degradation criterion. Two sets of constant stiffness and variable stiffness open-hole composite laminates experimental specimens were placed, respectively. A tensile strength experiment was performed.The results show that the numerical simulation accurately captures the data from experiment. The tensile strength of variable stiffness open-hole composite laminates, compared with constant stiffness open-hole composite laminates, increases by 26.92%, and the damage evolution processes of both are significantly different. 国家自然科学基金(51521064;51675479;11402228);中央高校基本科研业务费专项资金(2017FZA4002)
[1] | GURDAL Z, OLMEDO R. In plane response of laminates with spatially varying fiber orientations-variable stiffness concept[J]. AIAA Journal, 1993, 31(4):751-758. |
[2] | WU C, GURDAL Z, STARNES J. Structural response of compression-loaded, tow-placed, variable stiffness panels[C]//43rd AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics and Materials Conference. Denver, CO:American Institute of Aeronautics and Astronautics Inc, 2002. |
[3] | LOPES C S, GURDAL Z, CAMANHO P P. Tailoring for strength of composite steered-fibre panels with cutouts[J]. Composites Part A:Applied Science and Manufacturing, 2010, 41(12):1760-1767. |
[4] | 马永前, 张淑杰, 许震宇. 纤维曲线铺放的变刚度复合材料层合板的屈曲[J]. 玻璃钢/复合材料, 2009(5):31-35. MA Y Q, ZHANG S J, XU Z Y. The bucking of variable-stiffness composite panels with curvilinear fiber format[J]. Fiber Reinforced Plastics/Composites, 2009(5):31-35(in Chinese). |
[5] | 邵冠军, 游有鹏, 缪群华. 复合材料开孔层合板的纤维铺放路径优化设计[J]. 玻璃钢/复合材料, 2006(4):31-34. SHAO G J, YOU Y P, MIAO Q H. Optimization of fiber placement path for composite laminates with open holes[J]. Fiber Reinforced Plastics/Composites 2006(4):31-34(in Chinese). |
[6] | 谢丽婷, 祖磊, 王继辉, 等. 拉伸载荷下开孔层合板的纤维铺放轨迹研究[J]. 固体火箭技术, 2016, 39(2):247-252. XIE L T, ZU L, WANG J H, et al. Structural research on the fiber placing trajectory of open-hole composite laminate under tensile load[J]. Journal of Solid Rocket Technology, 2016, 39(2):247-252(in Chinese). |
[7] | 师春燕. 曲线铺放层合板结构设计与数值分析[D]. 西安:西安理工大学, 2013. SHI C Y. Structural design and numerical analysis on curvilinear placement laminates[D]. Xi'an University of Technology, 2013(in Chinese). |
[8] | HUHNE C, ZERBST A K, KUHLMANN G, et al. Progressive damage analysis of composite bolted joints with liquid shim layers using constant and continuous degradation models[J]. Composite Structures, 2010, 92(2):189-200. |
[9] | 谢宗蕻, 李想, 郭家平, 等. 各向异性复合材料开孔板拉伸强度预测及模型验证[J]. 复合材料学报, 2016, 33(6):1242-1250. XIE Z H, LI X, GUO J P, et al. Tensile strength prediction and model validation of anisotropic composite laminates with open holes[J]. Acta Materiae Compositae Sinica, 2016, 33(6):1242-1250(in Chinese). |
[10] | 卢子兴, 徐强, 王伯平, 等. 含缺陷平纹机织复合材料拉伸力学行为数值模拟[J]. 复合材料学报, 2011, 28(6):200-207. LU Z X, XU Q, WANG B P, et al. Numerical simulation of plain weave composites with defects under unidirectional tension[J]. Acta Materiae Compositae Sinica, 2011, 28(6):200-207(in Chinese). |
[11] | 鲍宏琛, 刘广彦. 准各向同性纤维增强复合材料层合板的开孔拉伸破坏模拟[J]. 复合材料学报, 2016, 33(5):1026-1032. BAO H C, LIU G Y. Simulation on damage in quasi-isotropic fiber-reinforced composite laminates under open-hole tension[J]. Acta Materiae Compositae Sinica, 2016, 33(5):1026-1032(in Chinese). |
[12] | 孔祥宏, 王志瑾. 基于Abaqus的有限元渐进损伤强度分析[J]. 计算机应用与软件, 2012(10):236-240. KONG X H, WANG Z J. Finite element incremental damage strength analysis based on ABAQUS[J]. Computer Application and Software, 2012(10):236-240(in Chinese). |
[13] | HYER M W, CHARETTE R F. Use of curvilinear fiber format in composite structure[J]. AIAA Journal, 1991, 29(6):1011-1015. |
[14] | GLIESCHE K, HUBNER T, ORAWETZ H. Application of the tailored fibre placement (TFP) process for a local reinforcement on an "open-hole" tension plate from carbon/epoxy laminates[J]. Composites Science and Technology, 2003, 63(1):81-88. |
[15] | IJSSELMUIDEN S T, ABDALLA M M, GURDAL Z. Thermomechanical design optimization of variable stiffness composite panels for buckling[J]. Journal of Thermal Stresses, 2010, 33(10):977-992. |