Postbuckling behaviour of square compression loaded graphite epoxy panels with square and elliptical cut-outs

被引:8
作者
Bailey, R [1 ]
Wood, J
机构
[1] Glasgow Caledonian Univ, Dept Engn, Glasgow G4 0BA, Lanark, Scotland
[2] Univ Paisley, Dept Mech & Mfg Engn, Paisley PA1 2BE, Renfrew, Scotland
关键词
D O I
10.1016/S0263-8231(97)00052-9
中图分类号
TU [建筑科学];
学科分类号
0813 ;
摘要
This paper investigates the influence of cutout shape, size and orientation upon the buckling stability of square CFRP panels. The study undertaken uses the ANSYS Finite Element Code for eigenvalue buckling and the postbuckling responses of the panels. Square panels with clamped edge conditions under displacement loading are considered. Results for square, circular and elliptical cutouts under uniaxial loading are presented. The results are shown for 300 mm square, 2.1 mm thick, 16-ply, quasi-isotropic (0/90/ +/- 45)(2s) panels with centrally and eccentrically located cutouts. (C) 1998 Elsevier Science Ltd. All rights reserved.
引用
收藏
页码:373 / 397
页数:25
相关论文
共 30 条
  • [11] MARSHALL IH, 1984, REINF PLAST C BRIGHT
  • [12] MARSHALL IH, 1986, P I MECH ENG
  • [13] MARSHALL IH, 1986, P REINF PLAST C NOTT, P91
  • [14] MARSHALL IH, 1987, 6 INT C COMP MAT ICC, V5
  • [15] MARTIN J, 1972, THESIS CASE W RESERV
  • [16] BUCKLING BEHAVIOR OF COMPRESSION-LOADED SYMMETRICALLY LAMINATED ANGLE-PLY PLATES WITH HOLES
    NEMETH, MP
    [J]. AIAA JOURNAL, 1988, 26 (03) : 330 - 336
  • [17] NEMETH MP, 1990, TP3024 NASA
  • [18] NEMETH MP, 1990, TP3007 NASA
  • [19] NEMTH MP, 1984, 86263 NASA TM
  • [20] NEMTH MP, 1983, THESIS VIRGINIA POLY