欢迎登录材料期刊网

材料期刊网

高级检索

建立了一个有效计算模型,以分析碳纤维复合材料层合板在低速冲击作用下的层内和层间失效行为.针对铺层板的层内损伤,在基于应变描述的Hashin失效准则的基础上,建立了单层板的逐渐累积损伤分析模型;针对铺层板的脱层损伤,建立了各向同性脱层损伤模型,通过结合传统的应力失效准则和断裂力学中的能量释放率准则定义了界面损伤演化规律,并在潜在产生脱层的区域模拟为粘结接触,并将脱层损伤模型作为界面的接触行为.该计算模型通过商用有限元软件ABAQUS/Explicit的用户子程序实现.使用该计算模型对碳纤维增强环氧树脂复合材料层合板在横向低速冲击作用下的损伤和变形行为进行预测分析.数值仿真的结果与试验结果进行了比较,取得了满意的结果,验证了该模型的正确性.

参考文献

[1] 王熙,卢国兴,余同希.复合材料管状结构的能量吸收性能[J].工程力学,2003,20(3):155-160.Wang Xi,Lu Guoxing,Yu Tongxi.Energy absorption behavior of composite tube structures[J].Engineering Mechanics,2003,20(3):155-160.
[2] Feraboli Paolo,Masini Attilio.Development of carbon/epoxy structural components for a high performance vehicle[J].Composites Part B:Engineering,2004,35(4):323-330.
[3] Hou J P,Petrinic N,Ruiz C,et al.Prediction of impact damage in composite plates[J].Composites Science and Technology,2000,60(2):273-281.
[4] Choi H Y,Chang F K.A model for predicting damage in graphite/epoxy laminated composites resulting from lowvelocity point impact[J].Journal of Composite Materials,1992,26(14):2134-2169.
[5] 李晨锋,程建钢,胡宁,等.模拟长纤维增强树脂层合板冲击损伤的数值方法[J].力学学报,2002,34(6):989-996.Li Chenfeng,Cheng Jiangang,Hu Ning,et al.A numerical simulation for impact damage of long-fiber reinforced resin laminates[J].Acta Mechanica Sinica,2002,34(6):989-996.
[6] Johnson A F,Pickett A K,Rozycki P.Computational meth ods for predicting impact damage in composite structures[J].Composites Science and Technology,2001,61(15):2183-2192.
[7] De Moura MFSF,Goncalves J P M.Modeling the interaction between matrix cracking and delamination in carbon-epoxy laminates under low velocity impact[J].Composites Science and Technology,2004,64(7-8):1021-1027.
[8] De Moura MFSF,Marques A T.Prediction of low velocity impact damage in carbon-epoxy laminates[J].Composites Part A:Applied Science and Manufacturing,2002,33(3):361-368.
[9] Hashin Z.Failure criteria for unidirectional fiber composites[J].Journal of Applied Mechanics,1980,47(2):329-334.
[10] Huang Chien Hua,Lee Ya Jung.Experiments and simulation of the static contact crush of composite laminated plates[J].Composite Structures,2003,61 (3):265-270.
[11] Zheng S,Sun C T.A double-plate finite-element model for the impact-induced delamination problem[J].Composites Science and Technology,1995,53(1):111-118.
[12] Borg R,Nilsson L,Simonsson K.Modeling of delamination using a discretized cohesive zone and damage formulation[J].Composites Science and Technology,2002,62(10-11):1299-1314.
[13] Zou Z,Reid S R,Li S.A continuum damage model for delaminations in laminated composites[J].Journal of Mechanics and Physics of Solids,2003,51(2):333-356.
[14] Borg Rikard,Nilsson Larsgunnar,Simonsson Kjell.Simulation of low-velocity impact on fiber laminates using a cohesive zone based delamination model[J].Composites Science and Technology,2004,64(2):279-288.
[15] Choi H Y,Wu H Y,Chang F K.A new 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(8):1012-1038.
[16] ABAQUS Analysis User's Manual[M].Version 6.4.2003.
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%