[1] Duncan W J. Galerkin's method in mechanics and differential equations, ADA951862[R].London:Aeronautical Research Council,1937. [2] Elishakoff I, Rollot O.New closed-form solutions for buckling of a variable stiffness column by Mathematica[J].Journal of Sound and Vibration,1999,224(1):172-182. [3] von Kármán T,Tsien H.The buckling of thin cylindrical shells under axial compression[J].Journal of the Aeronautics Science,1941,8(6):303-312. [4] Donnell L H, Wan C C.Effect of imperfections on buckling of thin cylinders and columns under axial compression[J].Journal of Applied Mechanics-transactions of the ASME,1950,17(1):73-83. [5] Koiter W T. The stability of elastic equilibrium,AD0704124[R].Standford:Department of Aeronautics and Astronautics of Standford University,1970. [6] Stein M. Some recent advances in the investigation of shell buckling[J].AIAA Journal,1968,6(12):2339-2345. [7] Kong C, Bang J,Sugiyama Y.Structural investigation of composite wind turbine blade considering various load cases and fatigue life[J].Energy,2005,30(11):2101-2114. [8] Rhead A T, Butler R,Hunt G W.Post-buckled propagation model for compressive fatigue of impact damaged laminates[J],International Journal of Solids and Structures,2008,45(16):4349-4361. [9] 李世荣,刘平. 弹性地基上Euler-Bernoulli梁的热屈曲模态跃迁特性[J].应用力学学报,2011,28(1):90-94. Li S R,Liu P.Thermal buckling mode transition characteristics of Euler-Bernoulli beam on the elastic foundation[J].Journal of Applied Mechanics,2011,28(1):90-94(in Chinese). [10] 贺尔铭,张钊, 胡亚琪,等.单轴压缩载荷下夹层梁结构屈曲及皱曲模拟研究[J].西北工业大学学报,2012,30(5):668-674. He E M,Zhang Z,Hu Y Q,et al.Buckling and wrinkling study of sandwich beam under uniaxial compression load[J].Journal of Northwestern Polytechnical University,2012,30(5):668-674(in Chinese). [11] 左志亮,蔡健, 朱昌宏.带约束拉杆L形钢管混凝土短柱的偏压试验研究[J].东南大学学报:自然科学版,2010,40(2): 346-351. Zuo Z L,Cai J,Zhu C H.Bias experimental study on the binding L-shaped concrete bars filled with steel tubes[J].Journal of Southeast University:Natural Sciences,2010,40(2):346-351(in Chinese). [12] 夏盛来,何景武, 海尔瀚.大展弦比机翼屈曲及后屈曲分析[J].机械强度,2012,33(6):907-912. Xia S L,He J W,Hai E H.Buckling and post-buckling analysis of the high aspect ration wing[J].Mechanics Strength,2012,33(6): 907-912(in Chinese). [13] 吴学仁. 飞机结构金属材料力学性能手册:静强度疲劳/耐久性[M].北京:航空工业出版社,1996:225-353. Wu X R.Manual of metal material mechanics performance of the plane structure:static fatigue strength/durability[M].Beijing:Aviation Industry Press,1996:225-353(in Chinese). [14] 王勖成. 有限单元法[M].北京:清华大学出版社,2003:649-651. Wang X C.The finite element method[M].Beijing:Tsinghua University Press,2003:649-651(in Chinese). [15] Lemaitre J, Desmorat R.Engineering damage mechanics:ductile,creep,fatigue and brittle failures[M].Berlin:Springer,2005:3-6. [16] 张行,崔德渝, 孟庆春.断裂与损伤力学[M].北京:北京航空航天大学出版社,2006:329-331. Zhang X,Cui D Y,Meng Q C.Fracture and damage mechanics[M].Beijign:Beijing University of Aeronautics and Astronautics Press,2006:329-331(in Chinese). [17] 张淼. 构件疲劳寿命预估的多变量损伤力学方法[D].北京:北京航空航天大学,2009. Zhang M.Multivariate fatigue damage mechanics methods of fatigue life prediction of the structure[D].Beijing:Beijing University of Aeronautics and Astronautics,2009(in Chinese). |