[1]杜凯繁,郝鹏,董曼红,等.非均匀刚度弹性边界结构优化设计及实验验证[J].固体火箭技术,2019,42(04):539-545.
 DU Kaifan,HAO Peng,DONG Manhong,et al.Optimization design for elastic boundary with non-uniform stiffness of cylindrical shells and experimental verification[J].Journal of Solid Rocket Technology,2019,42(04):539-545.
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非均匀刚度弹性边界结构优化设计及实验验证

参考文献/References:

[1]Priyadarsini R S,Kalyanaraman V,Srinivasan S M.Numerical and experimental study of buckling of advanced fiber composite cylinders under axial compression[J].Int.J.Struct.Stab.Dy.,2012,12(4):1250028-1-1250028-25.[2]Khakimova R,Wilckens D,Reichardt J,et al.Buckling of axially compressed CFRP truncated cones:experimental and numerical investigation[J].Compos.Struct.,2016,146:232-247.[3]Opoka S,Pietraszkiewicz W.On refined analysis of bifurcation buckling for the axially compressed circular cylinder[J].Int.J.Solids Struct.,2009,46(17):3111-3123.[4]Silvestre N.Buckling behaviour of elliptical cylindrical shells and tubes under compression[J].Int.J.Solids Struct.,2008,45(16):4427-4447.[5]Sutton M A,Cheng M,Peters W H,et al.Application of an optimized digital correlation method to planar deformation analysis[J].Image and Vision Computing.1986,4(3):143-50.[6]LUO P F,CHAO Y J,Sutton M A,et al.Accurate measurement of three-dimensional deformations in deformable and rigid bodies using computer vision[J].Experimental Mechanics,1993,33(2):123-132. [7]WANG B,DU K,HAO P,et al.Numerically and experimentally predicted knockdown factors for stiffened shells under axial compression[J].ThinWalled Structures,2016,109:13-24.[8]WANG B,ZHU S,HAO P,et al.Buckling of quasi-perfect cylindrical shell under axial compression:A combined experimental and numerical investigation[J].International Journal of Solids and Structures,2018,130-131:232-247.[9]Bisagni C.Composite cylindrical shells under static and dynamic axial loading:an experimental campaign[J].Prog.Aerosp.Sci.,2015,78:107-115.[10]王栋,刘丽坤,郑钢铁,弹性边界试验获取自由状态频响方法研究[J].航天器环境工程,2012,29(4):414-418.WANG D,LIU L K,ZHENG G T.Extraction of free body frequency response functions from elastically constrained test[J].Spacecraft Environment Engineering,2012,29(4):414-418.[11]HAO P,WANG B,LI G,et al.Hybrid framework for reliability-based design optimization of imperfect stiffened shells[J].AIAA Journal,2015,53(10),2878-2889.[12]WANG B,HAO P,LI G,et al.Generatrix shape optimization of stiffened shells for low imperfection sensitivity[J].Science China Technological Sciences,2014,57(10):2012-2019. [13]MENG Z,HAO P,LI G,et al.Non-probabilistic reliability-based design optimization of stiffened shells under buckling constraint[J].Thin-Walled Structures,2015,94:325-333.[14]HAO P,WANG B,TIAN K,et al.Efficient optimization of cylindrical stiffened shells with reinforced cutouts by curvilinear stiffeners[J].AIAA Journal,2016:54(4),1-14. [15]Lund E,Lindgaard E.Nonlinear buckling optimization of laminated composites including“worst”shape imperfections[J].Int.J.Solids Struct.,2010,47(22-23):3186-3202.[16]Barthelemy J F M, Haftka R T.Approximation concepts for optimum structural design-A review[J].Structural and Multidisciplinary Optimization,1993,5(3):129-144.[17]Cunha F R S D,Wille T,Degenhardt R,et al.A robustness-based design strategy for composite structures[J].Aircraft Engineering and Aerospace Technology,2014,86(4):687-687. [18]韩涵.运载火箭加筋壳结构稳定性分析[D].长沙:国防科学技术大学,2005.[19]郝鹏.面向新一代运载火箭的网格加筋柱壳结构优化研究[D].大连:大连理工大学,2013.[20]王斌.结构多性能优化设计及其在航天结构设计中的应用[D].大连:大连理工大学,2010.[21]HAO P,WANG B,LI G.Surrogate-based optimum design for stiffened shells with adaptive sampling[J].AIAA Journal,2012,50(11):2389-2407.[22]WANG B,HAO P,LI G,et al.Two-stage size-layout optimization of axially compressed stiffened panels[J].Structural and Multidisciplinary Optimization,2014,50(2):313-327.[23]HAO P,WANG B,TIAN K,et al.Fast procedure for Non-uniform optimum design of stiffened shells under buckling constraint[J].Structural and Multidisciplinary Optimization,2017,55(4):1503-1516.

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