欢迎登录材料期刊网

材料期刊网

高级检索

将复合材料细观力学桥联模型与有限元软件ABAQUS结合,用于分析层合板受低速冲击作用的极限承载能力.通过确定组分材料是否破坏来判断单层板是否破坏,对破坏后的单层实施一种常系数刚度衰减.将细观力学本构模型、针对组分材料的破坏判据以及刚度衰减模式编制成用户子程序VUMAT,为ABAQUS求解层合板的极限冲击响应提供一种自定义材料模型.只需要输入纤维和基体的材料参数、纤维体积含量等有限数据并且无须单层板的实验数据,就能顺利实施复合材料层合板结构的冲击承载能力分析.所计算的层合板的挠度-时间曲线以及横向冲击力-时间曲线与实验值吻合良好,说明本文的方法是有效的.

参考文献

[1] Abrate S .Impact on laminated composites:recent Advance[J].Applied Mechanics Reviews,1991,44(04):155-190.
[2] Ablate S .Impact on laminated composites:rencent Advance[J].Applied Mechanics Reviews,1994,47(11):517-544.
[3] 白瑞祥,陈浩然.低速冲击后含损复合材料夹层板剩余强度研究进展[J].力学进展,2002(03):402-414.
[4] 黄争鸣,张华山.纤维增强复合材料强度理论的研究现状与发展趋势--"破坏分析奥运会"评估综述[J].力学进展,2007(01):80-98.
[5] Hou JP;Petrinic N;Ruiz R .Prediction of impact damage in composite plates[J].Composites Science and Technology,2006,60:273-281.
[6] Chang F;Chang K .A progressive damage model for laminated composites containing stress concentrations[J].Journal of Composite Materials,1987,21:834-55.
[7] Brewer JC;Lagace PA .Quadratic stress criterion for initiation of delamination[J].Journal of Composite Materials,1988,22(12):1141-55.
[8] 程小全,郦正能.复合材料层合板低速冲击后压缩的损伤累积模型[J].应用数学和力学,2005(05):569-576.
[9] Chang FK;Springer GS .The strength of fiber reinforced composite bends[J].Journal of Composite Materials,1986,20:30-45.
[10] Hashin Z .failure ctiteria for unidirectional fiber composites[J].Journal of Applied Mechanics,Transactions of the ASME,1980,47:329-334.
[11] Zueleyha Aslan;Ramazan Karakuzu;Buket Okutan .The response of laminated composite plates under low-velocity impact loading[J].Composite Structures,2003(1):119-127.
[12] Choi HY;Wu HYT;Chang FK .A now approach toward understanding damage mechanisms and mechanics of laminated composites due-to low-velocity impact:part Ⅱ-analysis[J].Journal of Composite Materials,1991,25:1012-38.
[13] Choi HY;Chang FK .A mode for predicting damage in graphite/epoxy laminated composites resulting from low velocity point impact[J].Journal of Composite Materials,1992,26(14):2134-69.
[14] Johnson HE;Louca LA;Mooring SE .Current research into modelling of shock damage to large scale composite panels[J].Journal of Materials Science,2006(20):6655-6672.
[15] Mayes SJ;Hanaen AC .Composite laminate failure analysis using muhicentinuum theory[J].Composites Science and Technology,2004,64:379-394.
[16] Gotsis PK;Chamis CC;Minnetyan L .Prediction of composite laminate fracture:mieromechanics and progressive frature[J].Composites Science and Technology,1998,58:1137-1150.
[17] 田峰.塑性细观力学模型的比较分析[J].北京理工大学学报,1996(05):477.
[18] 黄争鸣.复合材料细观力学引论[M].北京:科学出版社,2004:49-60.
[19] 徐颖,温卫东,崔海坡.复合材料层合板低速冲击逐渐累积损伤预测方法[J].材料科学与工程学报,2006(01):77-81.
[20] Abaqus Analysis User Manual,version 6.4[M].
[21] J. P. Hou;N. Petrinic;C. Ruiz .A delamination criterion for laminated composites under low-velocity impact[J].Composites science and technology,2001(14):2069-2074.
[22] Collombet F;l.albin X;Latailade JL .Impact of laminated composites:physical basis for finite element analysis[J].Composites Science and Technology,1998,58:463-478.
上一张 下一张
上一张 下一张
计量
  • 下载量()
  • 访问量()
文章评分
  • 您的评分:
  • 1
    0%
  • 2
    0%
  • 3
    0%
  • 4
    0%
  • 5
    0%