Fatigue failure model for composite laminates under multi-axial cyclic loading

被引：0
|
作者：
Lee, C.S.
Hwang, W.
Park, H.C.
Han, K.S.
机构：
来源：
Key Engineering Materials | 2000年 / 183 (II卷
关键词：
Composite laminates - Fatigue modulus;
D O I：
暂无
中图分类号：
学科分类号：
摘要：
引用
收藏
页码：945 / 950
相关论文
共 50 条
  • [21] Predicting residual stiffness of cracked composite laminates subjected to multi-axial inplane loading
    Kashtalyan, M.
    Soutis, C.
    JOURNAL OF COMPOSITE MATERIALS, 2013, 47 (20-21) : 2513 - 2524
  • [22] Residual Stiffness of Cracked Cross-Ply Composite Laminates Under Multi-Axial In-plane Loading
    Soutis, Costas
    Kashtalyan, Maria
    APPLIED COMPOSITE MATERIALS, 2011, 18 (01) : 31 - 43
  • [23] Residual Stiffness of Cracked Cross-Ply Composite Laminates Under Multi-Axial In-plane Loading
    Costas Soutis
    Maria Kashtalyan
    Applied Composite Materials, 2011, 18 : 31 - 43
  • [24] Dynamic crack propagation in nano-composite thin plates under multi-axial cyclic loading
    Alshamma, Fathi A.
    Jassim, Omar Ali
    JOURNAL OF MATERIALS RESEARCH AND TECHNOLOGY-JMR&T, 2019, 8 (05): : 4672 - 4681
  • [25] Failure mechanisms of a notched CFRP laminate under multi-axial loading
    Tan, J. L. Y.
    Deshpande, V. S.
    Fleck, N. A.
    COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING, 2015, 77 : 56 - 66
  • [26] A FAILURE CRITERION FOR MULTI-AXIAL FATIGUE STRESSES
    STULEN, FB
    CUMMINGS, HN
    PROCEEDINGS-AMERICAN SOCIETY FOR TESTING AND MATERIALS, 1954, 54 : 822 - 835
  • [27] A tunnelling crack density evolution model for FRP laminates subjected to cyclic multi-axial strain-controlled loading
    Moncy, A.
    Castro, O.
    Glud, J.
    Berggreen, C.
    Thomsen, O. T.
    Dulieu-Barton, J. M.
    INTERNATIONAL JOURNAL OF SOLIDS AND STRUCTURES, 2023, 282
  • [28] Estimation method for fatigue life of notched specimen under multi-axial loading
    Wu, Zhi-Rong
    Hu, Xu-Teng
    Song, Ying-Dong
    Gongcheng Lixue/Engineering Mechanics, 2014, 31 (10): : 216 - 221
  • [29] A stiffness degradation model for composite laminates under fatigue loading
    Whitworth, HA
    COMPOSITE STRUCTURES, 1997, 40 (02) : 95 - 101
  • [30] A damage model based on the critical plane to estimate fatigue life under multi-axial random loading
    Gao, Dai-yang
    Yao, Wei-xing
    Wu, Tao
    INTERNATIONAL JOURNAL OF FATIGUE, 2019, 129
12345