参考文献/References:
[1] STEIN M. Nonlinear theory for plates and shells including the effects of transverse shearing[J]. AIAA journal, 1986, 24(9):1537-1544.
[2] 王林, 李峰, 田冀锋. 初始缺陷对耐压圆柱壳结构极限承载力的影响[J]. 江苏科技大学学报(自然科学版), 2009, 23(1):1-4.WANG Lin, LI Feng, TIAN Jifeng. Effects of initial defects to the limit load of pressure cylinder shell[J]. Journal of Jiangsu University of Science and Technology (natural science edition), 2009, 23(1):1-4.
[3] PASTUSZAK P D. Characterization of defects in curved composite structures using active infrared thermography[J]. Procedia engineering, 2016, 157:325-332.
[4] KHOT N S. Buckling and postbuckling behavior of composite cylindrical shells under axial compression[J]. AIAA journal, 1970, 8(2):229-235.
[5] 闫光, 韩小进, 阎楚良, 等. 复合材料圆柱壳轴压屈曲性能分析[J]. 复合材料学报, 2014, 31(3):781-787.YAN Guang, HAN Xiaojin, YAN Chuliang, et al. Buckling analysis of composite cylindrical shell under axial compression load[J]. Acta materiae compositae sinica, 2014, 31(3):781-787.
[6] 郝鹏, 王博, 李刚, 等. 基于缺陷敏感性分析的加筋圆柱壳结构设计[J]. 应用力学学报, 2013, 30(3):344-349.HAO Peng, WANG Bo, LI Gang, et al. Structural design of stiffened shells based on imperfection sensitivity analysis[J]. Chinese journal of applied mechanics, 2013, 30(3):344-349.
[7] YANG Jinshui, MA Li, CHAVES-VARGAS M, et al. Influence of manufacturing defects on modal properties of composite pyramidal truss-like core sandwich cylindrical panels[J]. Composites science and technology, 2017, 147:89-99.
[8] HÖRRMANN S, ADUMITROAIE A, SCHAGERL M. Through-thickness fatigue behavior of non-crimp fabrics featuring manufacturing defects[J]. Procedia structural integrity, 2016, 2:158-165.
[9] DAVIDSON P, WAAS A M. The effects of defects on the compressive response of thick carbon composites:an experimental and computational study[J]. Composite structures, 2017, 176:582-596.