Eiblmeier J, Loughlan J. The buckling response of carbon fiber composite panels with reinforced cut-outs J]. Composite Structures, 1995, 32:97-113.
[2]
Mahdi S, Kinloch A J, Matthews F L, Crisfield M A. The mechanical performance of repaired stiffened panels Ⅰ : Experimental characterization J]. Composites, 2002, 33:343-354.
[3]
Mahdi S, Kinloch A J, Crisfield M A. The mechanical performance of repaired stiffened panels Ⅱ : Finite element modeling J]. Composites, 2002, 33:355-366.
[4]
Marie laure Dano, Guy Gendron, Andre Picard. Stress and failure analysis of mechanically fastened joints in composite laminates J]. Composite Structures, 2000, 50: 287-296.
[5]
O’Neill G S.Asymmetric Reinforcements of a Quasiisotropic Graphite Epoxy Plate Containing a Circular Hole R].AD-A119625MF,1985.
[6]
Pickett D H, Sillivan P. Analysis of Symmetric Reinforcement of Quasi-isotropic Graphite/Epoxy Plates with a Circular Cutout under Uniaxial Tension Loading R]. AD-A139998MF, 1988.
[7]
程乐锦,薛明德,胡 宁. 基于三维有限元法的层合圆柱壳应力分析 J]. 复合材料学报,2003,20 ( 2):88-93. Cheng Lejin, Xue Mingde, Hu Ning. Stress analysis of the laminated cylindrical shells based on the 3D FEM J]. Acta Materiae Compositae Sinica, 2003, 20 ( 2):88-93.
[8]
罗小东, 寇长河, 于卫东. 复合材料层合结构开口的非对称补强研究 J]. 航空学报, 1994,15 ( 12): 1478-1481. Luo Xiaodong, Kou Changhe, Yu Weidong. Asymmetric submerged reinforcement of composite laminates containing a circular hole J]. Acta Aeronautica et Astronautica Sinica, 1994, 15 ( 12): 1478-1481.
[9]
寇长河, 汪 彤, 郦正能, 杨 旭. 复合材料层合板开口补强研究 J]. 北京航空航天大学学报, 1997,23 ( 4): 477-481. Kou Changhe, Wang Tong, Li Zhengneng, Yang Xu. Reinforcement research of composite laminates containing a circular hole J]. Journal of Beijing University of Aeronautics and Astronautics, 1997, 23 ( 4): 477-481.