刘丰睿, 赵丽滨.复合材料舱段三维应力分析及设计[J].材料工程, 2008, 52(5): 449-450. Liu Fengrui, Zhaolibin.Analysis and design of three-dimension stress of composite material cabin[J].Materials Engineering, 2008, 52(5): 449-450.
[2]
Miki M. Optimum fiber orientation angle of multi-axially laminated composites based on reliability[J].Reliability Engineering and System Safety, 2007, 66(3): 279-285.
[3]
Kogiso N, Murotsu Y. Effect of correlation on reliability based design of composite plate[J].Journal of Engineering Mechanics, 2003, 41(8): 717-724.
[4]
Murotsu Y, Shao S. Reliability design of fiber reinforced composites[J].Computers and Structures, 2004, 25(2): 145-151.
[5]
Kam Y. Reliability formulation for composite laminates subjected to first-ply failure[J].Composites Science and Technology, 2006, 47(6): 547-553.
[6]
Chen W. A compromise programming approach to robustness design[J].Advance in Design Automation, 2007, 121(3): 278-287.
[7]
Reneud E. Robustness design through minimum sensitivity[J].Journal of Composite Materials, 2007, 45(7): 667-677.
[8]
Sundaresen W. A robustness optimization procedure with variations on design constrains[J].Structural Optimization, 2007, 28(3): 283-291.
[9]
陈 晓, 许 可, 戴诗亮.求解层合板非线性屈曲问题一般方法的若干讨论[J].工程力学, 2002, 19(1): 73-78. Chen Xiao, Xu Ke, Dai Shiliang.Discussion on the general method for solution of nonlinear buckling problems of laminated plates[J].Engineering Mechanics, 2002, 19(1): 73-78.
[10]
Feng J. Composite material technology in the application of modern aircraft[J].Aviation Manufacturing Technology, 2009, 37(3): 251-262.
[11]
Rackwitz R, Fiessler M. The response of fibre metal laminates panels subjected to uniformly distributed loading[J]. European Journal of Mechanics-A/Solids, 2009, 42(2): 167-175.
[12]
关志东, 黎增山, 刘德博.复合材料层板开孔压缩损伤分析[J].复合材料学报, 2012, 29(3): 167-172. Guan Zhidong, Li Zengshan, Liu Debo.Damage analysis of open-hole compression laminates[J].Acta Materiae Compositae Sinica, 2012, 29(3): 167-172.
[13]
原梅妮, 杨延清, 李茂华.SiC/Ti-6Al-4V复合材料在横向拉伸载荷下界面失效行为的数值模拟[J].复合材料学报, 2012, 29(6): 159-163. Yuan Meini, Yang Yanqing, Li Maohua.Numerical simulation of the interface failure mechanism of SiC/Ti-6Al-4V composites under the transverse tensile stress[J].Acta Materiae Compositae Sinica, 2012, 29(6): 159-163.
[14]
刘德博, 关志东, 李 星.基于界面单元的复合材料Ⅱ型层间损伤分析[J].复合材料学报, 2012, 29(5): 151-156. Liu Debo, Guan Zhidong, Li Xing.Mode Ⅱ interlaminar damage analysis of composite laminates based on cohesive elements[J]. Acta Materiae Compositae Sinica, 2012, 29(5): 151-156.
[15]
高维成, 李小乐, 刘 伟.剪切载荷下含椭圆形大开口层合板的试验研究[J].复合材料学报, 2012, 29(6): 243-248. Gao Weicheng, Li Xiaole, Liu Wei.Experimental study on composite laminate with a large elliptical cutout under shear load[J].Acta Materiae Compositae Sinica, 2012, 29(6): 243-248.
[16]
Liu K S, Tsai S. Analytical fuselage and wing estimation of transport aircraft[J].Technical Memorandum, 2009, 32(5): 465-470.
[17]
Chenetal Y. A coordination design method to robustness design[J].Advance Design, 2005, 67(4): 368-376.
[18]
Zhang Y K.Composite structural optimization design of composite material cabin[J].Xibei Engineering University Journal, 2008, 51(11): 1048-1050.
[19]
Heimbs S, Vogt D, Hartnack R. Numerical simulation and optimization of aircraft interior components under loads[J].International Journal of Crashworthiness, 2008, 26(5): 511-521.
[20]
冯消冰, 黄 海, 王 伟.基于遗传算法的大型风机复合材料叶片根部强度优化设计[J].复合材料学报, 2012, 29(5): 196-202. Feng Xiaobing, Huang Hai, Wang Wei.Strength optimization of large wind turbine blade root on the genetic algorithm[J]. Acta Materiae Compositae Sinica, 2012, 29(5): 196-202.
[21]
Kogi N, Murot Y. Probabilistic failure analysis of loaded laminated composite structure using experiment method and first-order moment theory[J].Journal of Reinforced Plastics and Composites, 2002, 36(9): 892-905.