复合材料层合板缺口强度的CDM三维数值模型

李秋漳, 姚卫星, 陈方

李秋漳, 姚卫星, 陈方. 复合材料层合板缺口强度的CDM三维数值模型[J]. 复合材料学报, 2016, 33(12): 2766-2774. DOI: 10.13801/j.cnki.fhclxb.20160328.001
引用本文: 李秋漳, 姚卫星, 陈方. 复合材料层合板缺口强度的CDM三维数值模型[J]. 复合材料学报, 2016, 33(12): 2766-2774. DOI: 10.13801/j.cnki.fhclxb.20160328.001
LI Qiuzhang, YAO Weixing, CHEN Fang. CDM three-dimensional numerical model for notched strength of composite laminates[J]. Acta Materiae Compositae Sinica, 2016, 33(12): 2766-2774. DOI: 10.13801/j.cnki.fhclxb.20160328.001
Citation: LI Qiuzhang, YAO Weixing, CHEN Fang. CDM three-dimensional numerical model for notched strength of composite laminates[J]. Acta Materiae Compositae Sinica, 2016, 33(12): 2766-2774. DOI: 10.13801/j.cnki.fhclxb.20160328.001

复合材料层合板缺口强度的CDM三维数值模型

基金项目: 国家自然科学基金(11202098)
详细信息
    通讯作者:

    姚卫星,博士,教授,研究方向为飞行器综合设计和结构设计。E-mail:wxyao@nuaa.edu.cn

  • 中图分类号: TB330.1;V214.8

CDM three-dimensional numerical model for notched strength of composite laminates

  • 摘要: 针对复合材料层合结构缺口强度问题,基于连续损伤力学(CDM)提出了一种三维损伤数值模型。模型区分了层内损伤(纤维失效、纤维间失效)和层间分层损伤的不同失效模式。采用三维Puck准则与Aymerich准则对上述2类损伤进行判定,材料失效后基于CDM中线性软化模型对材料损伤进行演化。模型考虑了复合材料层合板子层的就位效应和剪切非线性行为。对Carlsson的AS4/3501-6缺口拉伸强度试验进行数值模拟。结果表明:分析结果与试验结果吻合良好,证明了该模型能够准确地预测含缺口复合材料层合板面内拉伸强度。
    Abstract: A three-dimensional damage numerical model was proposed based on continuum damage mechanics (CDM) to deal with problem of the notched strength of composite laminates. This model was able to distinguish different failure modes of in-plane damage (fiber failure, inter fiber failure) and interlaminar delamination damage. Three-dimensional Puck criterion and Aymerich criterion were used to judge two kinds of damage above. The damage was evolved based on the linear softening model of CDM after material failure. The in-situ effect and the shear nonlinear behavior of composite laminate sublayers were considered in the model. The tensile strength of notched AS4/3501-6 laminate tested by Carlsson was numerical simulated. The results show that the analysis results are in good agreement with the test results. The analysis results prove that the present model is capable of predicting the in-plane tensile strength of notched composite laminates.
  • 期刊类型引用(5)

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    2. 钱若力,许诺,王轩,周春苹,丁常方. 考虑就位效应的大开口层合板拉伸失效预测. 兵器材料科学与工程. 2020(02): 103-108 . 百度学术
    3. 杨凤祥,陈静芬,陈善富,刘志明. 基于剪切非线性三维损伤本构模型的复合材料层合板失效强度预测. 复合材料学报. 2020(09): 2207-2222 . 本站查看
    4. 拓宏亮,马晓平,卢智先. 含中心圆孔复合材料层合板失效分析及强度预测研究. 航空工程进展. 2018(02): 259-266 . 百度学术
    5. 曹倩妮,刘广彦,黄广炎. 组合载荷下含缺口纤维增强树脂基复合材料的失效分析. 复合材料学报. 2018(10): 2723-2729 . 本站查看

    其他类型引用(5)

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  • 被引次数: 10
出版历程
  • 收稿日期:  2015-12-14
  • 修回日期:  2016-03-18
  • 刊出日期:  2016-12-14

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