Strength predictions of finite width composite laminates containing a central circular hole

被引:0
|
作者
Harn, FE [1 ]
Han, FY [1 ]
机构
[1] Chongqing Inst Technol, Res Inst Composites, Sch Automobile Engn, Chongqing, Peoples R China
来源
JOURNAL OF ADVANCED MATERIALS | 2005年 / 37卷 / 04期
关键词
D O I
暂无
中图分类号
T [工业技术];
学科分类号
08 ;
摘要
The notched strength of a composite laminate containing a central circular cutout depends on material system, stacking sequence, hole size, and laminate width. Different layups and/or material systems may exhibit very different failure mechanisms. So far there are no globally accepted failure criteria developed for notched composite laminates. Four techniques of prediction of notched strengths of composite laminates are presented in this paper. Only the symmetric composite laminates containing one central hole under uniaxial tension are investigated in this paper. The techniques have revealed the influence of the variation of hole diameter-to-laminate width ratio (d/w) to the disparity of corresponding notched strength. It indicates that when d/w is greater than 0.3, the notched strength degrades almost linearly with increased d/w ratio. Good agreements have been observed between the proposed techniques and the test data adopted from literatures.
引用
收藏
页码:53 / 59
页数:7
相关论文
共 50 条
  • [31] Stress concentration in graphite/epoxy laminates containing a circular hole
    Whitworth, HA
    Mahase, H
    JOURNAL OF ADVANCED MATERIALS, 1999, 31 (04): : 45 - 51
  • [32] A study of 954-2A/IM7 composite laminates containing a central hole
    Kim, Hyungwon
    INTERNATIONAL JOURNAL OF MODERN PHYSICS B, 2008, 22 (9-11): : 1461 - 1468
  • [33] A new method for calculating of stitching reinforcement for composite laminates containing a large circular hole based on micromechanics
    Pan B.
    Zhang G.
    Sun Z.
    Guo W.
    Wang J.
    Xiao X.
    Fuhe Cailiao Xuebao/Acta Materiae Compositae Sinica, 2019, 36 (06): : 1447 - 1456
  • [34] STRESS-CONCENTRATION OF FINITE COMPOSITE LAMINATES WITH ELLIPTIC HOLE
    XU, XW
    SUN, LX
    FAN, XQ
    COMPUTERS & STRUCTURES, 1995, 57 (01) : 29 - 34
  • [35] Fracture strength of composite laminates containing surface notches
    Potti, PKG
    Rao, BN
    Srivastava, VK
    ADVANCED COMPOSITE MATERIALS, 2001, 10 (01) : 29 - 37
  • [36] STRAIN AND STRESS-CONCENTRATIONS IN COMPOSITE LAMINATES CONTAINING A HOLE
    TAN, SC
    KIM, RY
    EXPERIMENTAL MECHANICS, 1990, 30 (04) : 345 - 351
  • [37] SIMULATION OF MATRIX CRACKS IN COMPOSITE LAMINATES CONTAINING A SMALL HOLE
    REDDY, ES
    WANG, ASD
    ZHONG, Y
    JOURNAL OF REINFORCED PLASTICS AND COMPOSITES, 1990, 9 (02) : 104 - 117
  • [38] Tensile fracture of fibre reinforced metal laminates containing a circular hole
    Potti, PKG
    Rao, BN
    Srivastava, VK
    AERONAUTICAL JOURNAL, 2000, 104 (1031): : 47 - 51
  • [39] Fatigue life prediction and experiment research for composite laminates with circular hole
    Qi, HY
    Wen, WD
    Xun, LW
    JOURNAL OF CENTRAL SOUTH UNIVERSITY OF TECHNOLOGY, 2004, 11 (01): : 19 - 22
  • [40] Method for calculating the interlaminar stresses in symmetric laminates containing a circular hole
    Ko, Chu-Cheng
    Lin, Chien-Chang
    AIAA journal, 1992, 30 (01): : 197 - 204