Bisagni C, Cordisco P. An experimental investigation into the buckling and post-buckling of CFRP shells under combined axial and torsion loading [J]. Composite Structures, 2003, 60(4): 391-402.
[2]
Falzon B G, Steven G P. Buckling mode transition in hat-stiffened composite panels loaded in uniaxial compression [J]. Composites Structures, 1997, 37(2): 253-267.
[3]
Abramovich H, Weller T, Bisagni C. Buckling behavior of composite laminated stiffened panels under combined shear-axial compression [J]. Journal of Aircraft, 2008, 45(2): 402-413.
[4]
Falzon B G, Stevens K A, Davies G O. Postbuckling behaviour of a blade-stiffened composite panel loaded in uniaxial compression [J]. Composites Part A: Applied Science and Manufacturing, 2000, 31(5): 459-468.
[5]
Orifici A C, Shah S A, Herszberg I, et al. Failure analysis in postbuckled composite T-sections [J]. Composite Structures, 2008, 86(1-3): 146-153.
[6]
Stevens K A, Ricci R, Davies G A O. Buckling and postbuckling of composite structures [J]. Composites, 1995, 26(3): 189-199.
[7]
Oh S H, Kim K S, Kim C G. An efficient postbuckling analysis technique for composite stiffened curved panels [J]. Composite Structures, 2006, 74(3): 361-369.
[8]
Lynch C, Murphy A, Price M, et al. The computational post buckling analysis of fuselage stiffened panels loaded in compression [J]. Thin-Walled Structures, 2004, 42(10): 1445-1464.
[9]
Lanzi L. A numerical and experimental investigation on composite stiffened panels into post-buckling [J]. Thin-Walled Structures, 2004, 42(12): 1645-1664.
[10]
Liu P F, Hou S J, Chu J K, et al. Finite element analysis of postbuckling and delamination of composite laminates using virtual crack closure technique [J]. Composite Structures, 2011, 93(6): 1549-1560.
[11]
刘从玉, 许希武, 陈 康. 考虑脱粘的复合材料加筋板屈曲后屈曲及承载能力数值分析 [J]. 复合材料学报, 2010, 27(6): 158-166. Liu Congyu, Xu Xiwu, Chen Kang. Buckling, post-buckling and collapse analysis of stiffened composite panels with debonding damage [J]. Acta Materiae Compositae Sinica, 2010, 27(6): 158-166.
[12]
Jaberzadeh E, Azhari M. Elastic and inelastic local buckling of stiffened plates subjected to non-uniform compression using the galerkin method [J]. Applied Mathematical Modelling, 2009, 33(4): 1874-1885.
[13]
Ovesy H R, Assaee H. Buckling characteristics of some composite stiffened boxes under longitudinal compression or bending using finite strip approach [C] //44th AIAA/ASME/ASCE/AHS Structures, Structural Dynamics, and Materials Conference. Norfolk: AIAA, 2003: 1791.
[14]
Greenhalgh E, Meeks C, Clarke A, et al. The effect of defects on the performance of post-buckled CFRP stringer-stiffened panels [J]. Composites Part A: Applied Science and Manufacturing, 2003, 34(7): 623-633.
[15]
戴福隆, 沈观林, 谢惠民. 实验力学 [M]. 北京: 清华大学出版社, 2010: 390-411. Dai Fulong, Shen Guanlin, Xie Huimin. Mechanics of experiment [M]. Beijing: Tsinghua University Press. 2010: 390-411.
[16]
Benzeggagh M L, Kenane M. Measurement of mixed-mode delamination fracture toughness of unidirectional glass/epoxy composites with mixed-mode bending apparatus [J]. Composites Science and Technology, 1996, 56(4): 439-449.
[17]
Hilburger M W, Starnes Jr J H. Effects of imperfections of the buckling response of composite shells [J]. Thin-Walled Structures, 2004, 42(3): 369-397.
[18]
Degenhardt R, Kling A, Rohwer K, et al. Design and analysis of stiffened composite panels including post-buckling and collapse [J]. Computers & Structures, 2008, 86 (9): 919-929.