留言板

尊敬的读者、作者、审稿人, 关于本刊的投稿、审稿、编辑和出版的任何问题, 您可以本页添加留言。我们将尽快给您答复。谢谢您的支持!

姓名
邮箱
手机号码
标题
留言内容
验证码

不同冲击能量对层合板损伤及剩余强度的影响

崔海坡 温卫东 张阿龙

崔海坡, 温卫东, 张阿龙. 不同冲击能量对层合板损伤及剩余强度的影响[J]. 航空动力学报, 2015, 30(10): 2331-2337. doi: 10.13224/j.cnki.jasp.2015.10.005
引用本文: 崔海坡, 温卫东, 张阿龙. 不同冲击能量对层合板损伤及剩余强度的影响[J]. 航空动力学报, 2015, 30(10): 2331-2337. doi: 10.13224/j.cnki.jasp.2015.10.005
CUI Hai-po, WEN Wei-dong, ZHANG A-long. Influence of different impact energies on damage and residual strength of laminates[J]. Journal of Aerospace Power, 2015, 30(10): 2331-2337. doi: 10.13224/j.cnki.jasp.2015.10.005
Citation: CUI Hai-po, WEN Wei-dong, ZHANG A-long. Influence of different impact energies on damage and residual strength of laminates[J]. Journal of Aerospace Power, 2015, 30(10): 2331-2337. doi: 10.13224/j.cnki.jasp.2015.10.005

不同冲击能量对层合板损伤及剩余强度的影响

doi: 10.13224/j.cnki.jasp.2015.10.005
基金项目: 

国家自然科学基金(51305268)

详细信息
    作者简介:

    崔海坡(1978-),男,内蒙古赤峰人,副教授,博士,主要研究方向为材料设计、分析与应用.

  • 中图分类号: V214.8

Influence of different impact energies on damage and residual strength of laminates

  • 摘要: 基于三维逐渐损伤理论和全程分析方法,对复合材料层合板在冲击载荷及冲击后静载荷下的损伤过程进行分析,重点研究不同冲击能量对两种不同铺层参数、不同几何尺寸的T300/BMP-316复合材料层合板的损伤产生与扩展过程以及剩余强度的影响规律.结果表明:复合材料层合板存在可使其剩余强度急剧下降的冲击能门槛值.对于T300/BMP-316复合材料层合板而言,其冲击能量的门槛值介于5.0~5.5J之间;在冲击过程中,冲头下落速度具有一定的波动性,且不同铺层参数将影响冲击后复合材料层合板表面的凹痕深度.

     

  • [1] Asp L E,Nilsson S,Singh S.An experimental investigation of the influence of delamination growth on the residual strength of impacted laminates[J].Composites:Part A,2001,32(10):1229-1235.
    [2] Lee J,Soutis C.Prediction of impact-induced fibre damage in circular composite plates[J].Applied Composite Materials,2005,12(2):109-131.
    [3] Rikard B,Nilsson L,Simonsson K.Simulation of low velocity impact on fiber laminates using a cohesive zone based delamination model[J].Composites Science and Technology,2011,64(2):279-288.
    [4] Kashtalyan M,Soutis C.Stiffness and fracture analysis of laminated composites with off-axis ply matrix cracking[J].Composites:Part A,2007,38(4):1262-1269.
    [5] Davies G,Hitchings D,Wang J.Prediction of threshold impact energy for onset of delamination in quasi-isotropic carbon/epoxy laminated composites under low-velocity impact[J].Composites Science and Technology,2000,60(1):1-7.
    [6] Chen J F,Morozov E V,Shankar K.Simulating progressive failure of composite laminates including in-ply and delamination damage effects[J].Composites:Part A,2014,61(6):185-200.
    [7] Atas A,Mohamed G F,Soutis C.Modelling delamination onset and growth in pin loaded composite laminates[J].Composites Science and Technology,2012,72(10):1096-1101.
    [8] Zhang D T,Sun Y,Chen L,et al.A comparative study on low-velocity impact response of fabric composite laminates[J].Materials & Design,2013,50(9):750-756.
    [9] Chen J F,Morozov E V,Shankar K.A combined elastoplastic damage model for progressive failure analysis of composite materials and structures[J].Composite Structures,2012,94(12):3478-3489.
    [10] Chen A S,Almond D P,Harris B.Impact damage growth in composites under fatigue conditions monitored by acoustography[J].International Journal of Fatigue,2010,24(2/3/4):257-261.
    [11] Attia O,Kinloch A J,Matthews F L.The prediction of fatigue damage growth in impact-damaged composite skin/stringer structures:Part Ⅰ theoretical modeling studies[J].Composites Science and Technology,2011,63(10):1463-1472.
    [12] 赵渠森.先进复合材料手册[M].北京:机械工业出版社,2003.
    [13] CUI Haipo,WEN Weidong,CUI Haitao.Engineering approach for predicting post-impact compressive strength of laminated composites[J].Materials Science and Technology,2010,26(6):699-706.
    [14] 崔海坡,温卫东,崔海涛.复合材料层合板冲击损伤及剩余强度分析方法[J].固体力学学报,2006,27(3):237-242. CUI Haipo,WEN Weidong,CUI Haitao.Research on low velocity impact damage and residual strength of composite laminates[J].Acta Mechanica Solida Sinica,2006,27(3):237-242.(in Chinese)
    [15] 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.
    [16] Tserpes K I.Strength prediction of bolted joints in graphite/epoxy composite laminates[J].Composites:Part B,2002,33(5):521-529.
    [17] 崔海坡,温卫东,徐颖.复合材料板冲击损伤及剩余拉伸强度实验研究[J].航空动力学报,2007,22(10):1742-1747. CUI Haipo,WEN Weidong,XU Ying.Experimental research on impact damage and residual tensile strength of composite laminates[J].Journal of Aerospace Power,2007,22(10):1742-1747.(in Chinese)
    [18] 崔海坡,温卫东.T300/BMP316层合板冲击后压缩强度试验[J].航空动力学报,2008,23(11):2001-2006. CUI Haipo,WEN Weidong.Post-impact compressive strength experiment of T300/ BMP316 composite laminates[J].Journal of Aerospace Power,2008,23(11):2001-2006.(in Chinese)
  • 加载中
计量
  • 文章访问数:  1204
  • HTML浏览量:  3
  • PDF量:  679
  • 被引次数: 0
出版历程
  • 收稿日期:  2014-03-28
  • 刊出日期:  2015-10-28

目录

    /

    返回文章
    返回