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阐述了复合材料格栅结构稳定性及优化分析方法研究概况.指出在格栅结构初级设计阶段可利用拟膜分析法对等效的格栅平板、圆筒及锥筒进行整体屈曲计算即可,而对于复杂构型格栅结构,由于不对称性及拉-压-扭耦合效应存在很难获得解析解,需借助有限法对结构进行非线性求解而求得其真实力学响应,同时还介绍了其他算法,如遗传算法.最后介绍了复合材料格栅结构破坏机理的一些试验方法.

参考文献

[1] 燕瑛,刘玉佳,廖宝华,闫伟.先进复合材料格栅结构与大型飞机[J].航空制造技术,2009(02):26-29.
[2] 中国航空研究院.复合材料结构设计手册[M].北京:航空工业出版社,2011:356.
[3] Vasiliev V V;Barynin V A;Rain A F .Anisogrid lattice structures-survey of development and application[J].Computers & Structures,2001,54:361-370.
[4] V.V. Vasiliev;A.F. Razin .Anisogrid composite lattice structures for spacecraft and aircraft applications[J].Composite structures,2006(1/2):182-189.
[5] Totaro G;Gurdal Z .Optimal design of composite lattice shell structures for aerospace applications[J].Aerospace Science and Technology,2009,13:127-164.
[6] Slinchenko D;Verijenko V E .Structural analysis of composite lattice shells of revolution on the basis of smearing stiffness[J].Computers & Structures,2001,54:341-348.
[7] Ambur D R;Jaunky N .Optimal design of grid-stiffened panels and shells with variable curvature[J].Computers & Structures,2001,52:173-180.
[8] Kidane Samuel;Li Guoqiang et al.Buckling load analysis of grid stiffened composite cylinders[J].Composites Part B:Engineering,2003,34:1-9.
[9] 吴德财,徐元铭,贺天鹏.新的复合材料格栅加筋板的平铺等效刚度法[J].力学学报,2007(04):495-502.
[10] 李晶晶 .复合材料点阵结构承力筒设计与成型工艺研究[D].国防科学技术大学,2010.
[11] Wodesenbet Eyassu;Kidane Samuel;Pang Suseng .Optimization for buckling loads of grid stiffened composite panels[J].Computers & Structures,2003,60:159-169.
[12] Morozov E V;Lopatin A V;Nesterov V A.Buckling analysis and design of anisogrid composite lattice conical shells[J].Computers & Structures,2011:19.
[13] M. Buragohain;R. Velmurugan .Study of filament wound grid-stiffened composite cylindrical structures[J].Composite structures,2011(2):1031-1038.
[14] E. Frulloni;J. M. Kenny;P. Conti;L. Torre .Experimental study and finite element analysis of the elastic instability of composite lattice structures for aeronautic applications[J].Composite structures,2007(4):519-528.
[15] Prakash Jadhav;P. Raju Mantena .Parametric optimization of grid-stiffened composite panels for maximizing their performance under transverse loading[J].Composite structures,2007(3):353-363.
[16] E.V. Morozov;A.V. Lopatin .Design and analysis of the composite lattice frame of a spacecraft solar array[J].Composite structures,2011(7):1640-1648.
[17] 白瑞祥,王蔓,陈浩然.含损伤复合材料AGS板的屈曲特性[J].复合材料学报,2005(04):136-141.
[18] 何景轩,何国强,任明法.复合材料格栅结构屈曲特性分析[J].固体火箭技术,2008(04):389-392.
[19] 张志峰,陈浩然,李煊,蒋元兴.先进复合材料格栅圆柱壳优化设计的混合遗传算法[J].复合材料学报,2005(02):166-171.
[20] 提亚峰,董波,郭永辉,王婧超.C/E复合材料网格缠绕结构三维建模与模具设计[J].宇航材料工艺,2010(04):23-26,43.
[21] 荣晓敏,徐元铭,吴德财.进化神经网络在复合材料格栅结构设计中的应用[J].固体火箭技术,2006(04):305-309.
[22] Nikolaev V P;Pichugin V S;Korobeinikov A G .Effect of molding conditions on fracture mechanisms and stiffness of a composite of grid structure[J].Mechanics of Composite Materials,1999,35(01):49-53.
[23] Luca Lanzi .A numerical and experimental investigation on composite stiffened panels into post-buckling[J].Thin-Walled Structures,2004(12):1645-1664.
[24] Chiara Bisagni;Potito Cordisco .Post-buckling and collapse experiments of stiffened composite cylindrical shells subjected to axial loading and torque[J].Composite structures,2006(2):138-149.
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