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基于局部屈曲、压损载荷的帽型长桁截面优化设计 被引量:3

Optim izing the Hat-Stringer Cross Section Based on Local-Buckling and Crippling
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摘要 由于帽型长桁的截面尺寸较大,其两边突缘与蒙皮相连形成一个闭合截面,具有很高的受压稳定性,因此被广泛应用于复合材料机身壁板。在局部屈曲和压损载荷下,用MATLAB线性优化帽型长桁截面尺寸,并得出帽型长桁局部屈曲载荷与帽底宽度,帽腰和帽底夹角的关系曲线;压损载荷与帽底宽度,帽腰和帽底夹角的关系曲线,为设计师在初步尺寸设计时提供参考。 The hat-stringer has large cross section and the cross section is closed by flanges and skin,which leads to high stability when it compressed. For this reason the hat-stringer is widely used in composite panel. This paper optimizes the hat-stringer section in the condition of local-buckling and crippling by MATLAB,and obtaines the buckling strength as function of hat-stringer width and the angle between hat-stringer width and the waist,and the crippling strength as function of hat-stringer width and the angle between hat-stringer width and the waist. These functions can provide references to designers in the preliminary design.
作者 刘卫 何周理 LIU Wei;HE Zhouli(COMAC Beijing Aeronautical Science & Technology Research Institute,Beijing 102209,China;Shanghai Aircraft Design and Research Institute,Shanghai 201210,China)
出处 《民用飞机设计与研究》 2018年第2期85-89,共5页 Civil Aircraft Design & Research
关键词 帽型长桁 局部屈曲 压损 截面优化 hat-stringer local-buckling crippling optimization
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  • 1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. 被引量:14
  • 2Liu Wenli, Butler R. Optimum buckling design of composite wing cover panels with manufacturing constraints[R]. AIAA 2007-2215,2007.
  • 3Watson A, Featherston C A, Kennedy D. Optimization of postbuckled stiffened panels with multiple stiffener sizes[R]. AIAA 2007-2207,2007.
  • 4Iuspa L, Ruoeco E. Optimum topological design of simply supported composite stiffened panels via genetic algorithms[J]. Computers & Structures, 2008, 86(17/18) : 1718-1737.
  • 5Liu Wenli, Butler R, Mileham A R, et al. Optimum design, experimental testing and post-buckling analysis of thick composite stiffened panels[R]. AIAA 2005-1826, 2005.
  • 6Rikards R, Abramovich H, Kalnins K, et al. Surrogate modeling in design optimization of stiffened composite shells [J]. Composite Structures, 2006, 73: 244-251.
  • 7Todoroki A, Sekishiro M. Stacking sequence optimization to maximize the buckling load of blade-stiffened panels with strength constraints using the iterative fractal branch and bound method[J]. Composites, Part B Engineering, 2008,39 : 842-850.
  • 8Le Riche R, Haftka R T. Optimization of laminate stacking sequence for buckling load maximization by genetic algorithm [J]. AIAA Journal, 1993, 31 (5):951-956.
  • 9Soremekun G, Gurdal Z, Haftka R T, et al. Composite laminate design optimization by genetic algorithm with generalized elitist selection [J]. Computers & Structures, 2001,79:131-143.
  • 10Holland J H. Adaptation in natural and artificial systems [M]. Ann Arbor, MI: The University of Michigan Press, 1975.

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