[1] CALLADINE C R. Understanding imperfection-sensitivity in the buckling of thin-walled shells[J].Thin-Walled Structures, 1995, 23(1):215-235. [2] 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 P, WANG B, LI G, et al. Structural design of stiffened shells based on imperfection sensitivity analysis[J].Chinese Journal of Applied Mechanics, 2013, 30(3):344-349(in Chinese). [3] CAMPBELL J,HETEY L,VIGNJEVIC R. Nonlinear idealization error analysis of a metallic stiffened panel loaded in compression[J].Thin-Walled Structures, 2012, 54:44-53. [4] BERNARD E S,COLEMAN R,BRIDGE R Q. Measurement and assessment of geometrical imperfections in thin-walled panels[J].Thin-Walled Structures, 1999, 33:103-126. [5] LANZI L A. A numerical and experimental investigation on composite stiffened panels into post-buckling[J].Thin-Walled Structures, 2004, 42(12):1645-1664. [6] HOUSTON G, QUINN D, MYRPHY A, et al. Impact of geometric imperfections on metallic stiffened panels with skin bay buckling containment features[C]//53th AIAA/ASME/ASCE/AHS/ASC Structure, Structure Dynamics, and Materials Conference. Reston:AIAA, 2012. [7] PAULO R M F, TEIXEIRA-DIAS F, VALENTE R A F. Numerical simulation of aluminum stiffened panels subjected axial compression:Sensitivity analyses to initial geometrical imperfections and material properties[J].Thin-Walled Structures, 2013, 62(1):65-74. [8] XU M C, SOARES C G. Assessment of the ultimate strength of narrow stiffened panel tests specimens[J].Thin-Walled Structures, 2012, 55:11-21. [9] 刘存,张磊,杨卫平. 舰载机壁板剪切后屈曲承载能力预测与试验验证[J].航空学报, 2019, 40(4):622300. LIU C, ZAHNG L, YANG W P. Post-buckling study and test verification of carrier-based aircraft wing stiffened panels under shear load[J].Acta Aeronautica et Astronautica Sinica, 2019, 40(4):622300(in Chinese). [10] HILBURGER M W, NEMETH M P, STARNES J H. Shell buckling design criteria based on manufacturing imperfection signatures[J].AIAA Journal, 2006, 44(3):654-663. [11] HILBURGER M W, STARNES J H J. Effects of imperfections on the buckling response of compression-loaded composite shells[C]//41 st AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston:AIAA, 2000. [12] RIGO P, SARGHIUTA R, ESTEFEN S, et al. Sensitivity analysis on ultimate strength of aluminum stiffened panels[J].Marine Structures, 2003,16:437-468. [13] COUTO C, VILA R P. Numerical investigation on the influence of imperfections in the local buckling of thin-walled I-shaped sections[J].Thin-Walled Structures, 2019, 135:89-108. [14] SALTELLI A, RATTO M, TARANTOLA S, et al. Sensitivity analysis practices:Strategies for model-based inference[J].Reliability Engineering and System Safety, 2006, 91(10-11):1109-1125. [15] 罗鹏程,傅攀峰. 武器装备敏感性分析方法综述[J].计算机工程与设计, 2008, 29(21):5546-5549. LUO P C, FU P F. Review on weapons and equipment sensitivity analysis methods[J].Computer Engineering and Design, 2008, 29(21):5546-5549(in Chinese). [16] SALTELLI A, MARIVOET J. Non-parametric statistics in sensitivity analysis for model output:A comparison of selected techniques[J].Reliability Engineering System Safety, 1990, 28(2):229-253. [17] HELTON J C, DAVIS F J. Survey of sampling-based methods for uncertainty and sensitivity analysis[J].Reliability Engineering System Safety, 2006, 91(10):1175-1209. [18] SOBOI I M. Global sensitivity indices for nonlinear mathematical models and their Monte Carlo estimates[J].Mathematics and Computers in Simulation, 2001, 55(1-3):271-280. [19] BORGONOVO E. A new uncertainty importance measure[J].Reliability Engineering System Safety, 2007, 92(6):771-784. [20] CUI L J, LU Z Z, ZHAO X P. Moment-independent importance measure of basic random variable and its probability density evolution solution[J].Science China Technological Sciences, 2010, 53(4):1138-1145. [21] LI L Y, LU Z Z, FENG J, et al. Moment-independent importance measure of basic variable and its state dependent parameter solution[J].Structural Safety, 2012, 38:40-47. [22] RICE R C, JACKSON J L, BAKUCKAS J, et al. Metallic materials properties development and standardization[M]. Washington,D. C.:Federal Aviation Administration, 2003:3-429. [23] LANZI L A, GIAVOTTO V O. Post-buckling optimization of composite stiffened panels computations and experiments[J].Composite Structures, 2006,73:208-220. [24] ABRAMOVICH H, BISAGNI C, CORDISCO P. Post-buckling test simulation of a stiffened composite panel[C]//48th AIAA/ASME/ASCE/AHS/ASC Structures, Structural Dynamics, and Materials Conference. Reston:AIAA, 2007. [25] ZHANG S M, KHAN I. Buckling and ultimate capability of plates and stiffened panels in axial compression[J].Marine Structures, 2009, 22(4):791-808. [26] XU M C, SOARES C G. Assessment of the ultimate strength of narrow stiffened panel tests specimens[J].Thin-Walled Structures, 2012, 55:11-21. [27] LI Y B, PAN Q, HUANG M H, et al. Set-based parametric modeling, buckling and ultimate strength estimation of stiffened ship structures[J].Journal of Central South University, 2019, 26(7):1958-1975. [28] MAZZOLAN M. Aluminum alloy structures[M]. Boston:Pitman, 1985. |