复合材料科学与工程 ›› 2026, Vol. 0 ›› Issue (7): 44-56.DOI: 10.19936/j.cnki.2096-8000.20260728.006

• 基础与力学性能研究 • 上一篇    下一篇

基于RVE模型的开孔层合板拉伸强度不确定性分析

李恩情1, 刘兴龙1, 宋挺1, 卢翔2*   

  1. 1.中国民航大学 航空工程学院,天津 300300;
    2.中国民航大学 交通科学与工程学院,天津 300300
  • 收稿日期:2025-06-06 出版日期:2026-07-28 发布日期:2026-08-06
  • 通讯作者: 卢翔(1969—),男,博士,教授,硕士生导师,研究方向为民机复合材料结构损伤与修理分析,xlu@cauc.edu.cn。
  • 作者简介:李恩情(2001—),女,硕士研究生,研究方向为航空复合材料不确定性分析。
  • 基金资助:
    国家自然科学基金 (U2433213)

Uncertainty analysis of tensile strength of open-hole laminates based on RVE modeling

LI Enqing1, LIU Xinglong1, SONG Ting1, LU Xiang2*   

  1. 1. College of Aerospace Engineering, Civil Aviation University of China, Tianjin 300300, China;
    2. College of Transportation Science and Engineering, Civil Aviation University of China, Tianjin 300300, China
  • Received:2025-06-06 Online:2026-07-28 Published:2026-08-06

摘要: 针对材料制备过程中纤维和孔隙不均匀导致开孔层合板力学性能分散性的问题,开发了一种随机分布纤维-基体-孔隙三相RVE模型的生成算法,进行了开孔层合板宏细观渐进损伤分析,并利用混沌多项式展开方法求解纤维与孔隙的尺寸(Rf,Rv)和体积分数(Vf,Vv)的灵敏度,实现了对开孔层合板拉伸强度的不确定性预测。分析结果表明:在Vf降低与Vv增加的综合影响下,开孔层合板的弹性性能参数最大降幅为29.47%,极限载荷降幅为14.51%,均显著超过单一参数(VfVv)变化引起的相应最大降幅(19.5%、10.94%)。对于开孔层合板失效位移,各参数影响排序为:Vf > Rf > Vv >Rv;对于开孔层合板极限载荷,各参数影响排序为:Vv > Vf > Rv > Rf。这表明体积分数变化影响均高于尺寸变化影响。

关键词: 开孔层合板, RVE模型, 力学性能, 混沌多项式展开, 不确定性

Abstract: Aiming at the problem of dispersion of mechanical properties of open-hole laminates due to fiber and pore inhomogeneity during material preparation, this study develops an algorithm for generating a three-phase RVE model with randomly distributed fibers-substrate-pores, performs macro- and fine-scale progressive damage analyses of open-hole laminates, and solves for the sensitivities of the dimensions of the fibers and pores (Rf, Rv) and the volume fractions (Vf, Vv) by using a polynomial chaos expansion method, to realize theuncertainty prediction of tensile strength of open-hole laminates.The analytical results show that under the combined effect of Vf decrease and Vv increase, the maximum decrease in the elastic performance parameters of the open pore plywood is 29.47%, and the ultimate load decrease is 14.51%, which are significantly more than the corresponding maximum decreases caused by the changes of a single parameter (Vf or Vv) by 19.5% and 10.94%, respectively. For the failure displacements of open-hole laminates, the parameter influences were ranked as Vf > Rf > Vv > Rv; for the ultimate loads of open-hole laminates, the parameter influences were ranked as Vv > Vf > Rv > Rf. Which showed that the effects of the changes in volume fraction were greater than the effects of the changes in dimensions.

Key words: open-hole laminate, RVE modeling, mechanical properties, polynomial chaos expansion, uncertainty

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