Fukunaga H, Vanderplaats G N. Stiffness optimization of orthotropic laminated composites using lamination parameters[J]. AIAA Journal, 1991, 29(4): 641-646.
[2]
Diaconu C G. Layup optimization for buckling of laminated composite shells with restricted layer angles[J]. AIAA Journal, 2004, 42(10): 2153-2163.
[3]
Liu B, Haftk R T. Single-level composite wing optimization based on flexural lamination parameters[J]. Structural and Multidisciplinary Optimization, 2004, 26: 111-120.
[4]
Herencia J E, Haftka R T, Weaver P M, et al. Lay-up optimization of stiffened panels using linear approximations in lamination spaces[J]. AIAA Journal, 2008, 46(9): 2387-2391.
[5]
Ijsselmuiden S T, Abdalla M M, Gürdal Z. Optimization of variable-stiffness panels for maximum buckling load using lamination parameters[J]. AIAA Journal, 2010, 48(1): 134-143.
晏 飞, 李为吉. 基于自适应遗传算法的复合材料层合板铺层顺序优化设计[J]. 西北工业大学学报, 2001, 19(1): 156-159. Yan Fei, Li Weiji. A stacking sequence optimization method of composite laminated panel based on an adaptive genetic algorithm[J]. Journal of Northwestern Polytechnical University, 2001, 19(1): 156-159.
[8]
鲁大伟, 李 书. 应用免疫遗传算法优化设计层合板铺层顺序[J]. 北京航空航天大学学报, 2005, 31(2): 247-250. Lu Dawei, Li Shu. Stacking sequence optimization of composite laminate applying genetic algorithm of immunity[J]. Journal of Beijing University of Aeronautics and Astronautics, 2005, 31(2): 247-250.
[9]
Kameyama M, Fukunaga H. Optimum design of composite plate wings for aeroelastic characteristics using lamination parameters[J]. Computers and Structures, 2007, 85(3): 213-224.
[10]
Thuwis G, Breuker R, Abdalla M, et al. Aeroelastic tailoring using lamination parameters[J]. Structural and Multidisciplinary Optimization, 2010, 41(4): 637-646.
[11]
李顺林, 王兴业. 复合材料结构设计基础[M]. 武汉: 武汉理工大学出版社, 2011: 45-47. Li Shunlin, Wang Xingye. Composite structure design foundation[M]. Wuhan: Wuhan University of Technology Press, 2011: 45-47.
[12]
MSC.Software Corporation. MSC/NASTRAN linear static analysis, user's guide.[M]. Los Angeles: MSC.Software Corporation Press, 2003: 217-234.
[13]
李为吉, 宋笔锋, 孙侠生, 等. 飞行器结构优化设计[M]. 北京: 国防工业出版社, 2005: 182-183. Li Weiji, Song Bifeng, Sun Xiasheng, et al. Structural optimization of aircraft[M]. Beijing: National Defence Industry Press, 2005: 182-183.
[14]
朱胜利, 姚雄华, 刘红武. 复合材料机翼翼盒结构多约束参数优化设计[C]//复合材料: 创新与可持续发展, 2010: 96-104. Zhu Shengli, Yao Xionghua, Liu Hongwu. Multidisciplinary sizing optimization design of a composite aircraft wing-box[C]//Composite Materials: Innovation and Sustainable Development, 2010: 96-104.
[15]
Shirk M H, Hertz T J, Weisshaar T A. Aeroelastic tailoring theory, practice, and promise[J]. Journal of Aircraft, 1986, 23(1): 6-18.
[16]
万志强, 杨 超. 利用MSC.Nastran 进行复合材料飞机的气动弹性剪裁设计[C]//MSC.Software中国用户论文集, 2002. Wan Zhiqiang, Yang Chao. Aeroelastic tailoring design of composite aircraft using MSC.Nastran.[C]//MSC.Software Users of China, 2002.
[17]
张桂江. 飞行器复合材料结构弹性刚度剪裁优化设计技术研究[D]. 西安: 西北工业大学航空学院, 2006. Zhang Guijiang. Optimal design techniques study with the elastic tailoring application of the aircraft composite structures[D]. Xi'an: School of Aeronautical, North-western Polytechnical University, 2006.
[18]
Weisshaar T A. Aeroelastic tailoring of forward swept composite wings[J]. Journal of Aircraft, 1981, 18(8): 669-676.
[19]
Librescu L, Song O. On the static aeroelastic tailoring of composite aircraft swept wings modeled as thin-walled beam structures[J]. Composite Engineering, 1992, 2(5-7): 492-517.
[20]
Meirovitch L, Seitz T L. Structural modeling for optimization of low aspect ratio composite wings[J]. Journal of Aircraft, 1995, 32(5): 1114-1123.
[21]
Lillico M. Aeroelastic optimization of composite wings using the dynamic stiffness method[J]. Aeronautical Journal, 1997, 101(1002): 77-86.
[22]
万志强, 杨 超, 郦正能. 混合遗传算法在气动弹性多学科优化中的应用[J]. 北京航空航天大学学报, 2004, 30(112): 1142-1146. Wan Zhiqiang, Yang Chao, Li Zhengneng. Application of hybrid genetic algorithm in aeroelastic multidisciplinary optimization[J]. Journal of Beijing University of Aeronautics and Astronautics, 2004, 30(112): 1142-1146.
[23]
刘 钢, 孙宪学, 陈文浦. 一种面向工程的气动弹性剪裁技术[J]. 航空计算技术, 2006, 36(5): 73-75. Liu Gang, Sun Xianxue, Chen Wenfu. A technique of engineering-oriented aeroelasticity tailoring aeronautical computing technique[J]. Aeronautical Computing Tech-nique, 2006, 36(5): 73-75.
[24]
谭申刚, 万志强. 基于现代优化方法的气动弹性建模与设计技术[J]. 工程力学, 2008, 25(8): 235-240. Tan Shengang, Wang Zhiqiang. Aeroelastic modeling and design technology based on modern optimization methods[J]. Engineering Mechanics, 2008, 25(8): 235-240.
[25]
王红伟, 王志瑾. 复合材料前掠翼的气动弹性优化[J]. 飞机设计, 2011, 31(4): 24-29. Wang Hongwei, Wang Zhijin. Aeroelastic optimization for forward-swept wing of composite material[J]. Aircraft Design, 2011, 31(4): 24-29.
[26]
晏 飞, 王利京. 带有气动弹性约束的复合材料翼面结构优化[C]//第七届全国空气弹性学术交流会, 2001: 146-159. Yan Fei, Wang Lijing. Composite wing structure optimization with aeroelastic constraints[C]//The 7th Aeroelastic Academic Exchange Proceeding, 2001: 146-159.
[27]
李为吉, 辜 曦. 复合材料结构的优化设计[J]. 宇航学报, 1990, 2(1): 35-43. Li Weiji, Gu Xi. Optimal design of composite structure[J]. Journal of Astronautics, 1990, 2(1): 35-43.
[28]
李太鹏, 徐元铭. 基于PATRAN/NASTRAN的复合材料结构铺层的分级优化设计方法[J]. 固体火箭技术, 2004, 27(4): 308-311, 315. Li Taipeng, Xu Yuanming. A multilevel optimization for layer design of composite structures based on PATRAN/NASTRAN[J]. Journal of Solid Rocket Technology, 2004, 27(4): 308-311, 315.
[29]
Riche L R, Haftka R T. Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm[J]. AIAA Journal, 1993, 31(5): 951-956.
[30]
修英姝, 崔德刚. 复合材料层合板稳定性的铺层优化设计[J]. 工程力学, 2005, 22(6): 212-216. Xiu Yingshu, Cui Degang. Ply optimization design for stability of composite laminates[J]. Engineering Mechanics, 2005, 22(6): 212-216.
[31]
杨智春, 张立新, 谭光辉. 基于遗传算法的复合材料壁板热颤振优化设计[J]. 宇航学报, 2008, 29(4): 1451-1456. Yang Zhichun Zhang Lixin, Tan Guanghui. Stacking sequence optimization of laminated composite panels for maximum flutter speed[J].Journal of Astronautics, 2008, 29(4): 1451-1456.
[32]
Miki M. Material design of composite laminates with required in-plane elastic properties[C]//Proceedings of the fourth International Conference on Composite Materials, 1982: 1725-1731.
[33]
Grenestedt J L, Gudmundson P. Layup optimization of composite material structures[C]//Proceedings of IUTAM Symposium on Optimal Design with Advanced Material, 1993: 311-336.
