对于复合材料加筋壁板稳定性优化问题,由于涉及多个设计变量:筋条数目、筋条间距、筋条高度、筋条的铺层参数、面板的铺层参数等,本文采用具有多参数级联编码方式的遗传算法时基于稳定性设计要求的加筋壁板进行了优化.对复合材料T型加筋壁板结构重量优化的算例,验证了本文所用方法的有效性.
参考文献
[1] | Venkataraman .Modeling,analysis and optimization of cylindrical stiffened panels for reusable launch vehicle structures[D].University of Florida,1999. |
[2] | Lueiano Lamberti;Satchi Venkataraman;Raphael T.Haftka.Comparison of preliminary designs of stiffened panels optimized u sin g PANDA2 for reusable launch vehicle propellant tan ks[J].AIAA Journal,2000 |
[3] | Bisagni C;Lanzi L.Post-buckling optimization of composite stiffened panels u sin g neural networks[J].Computers & Structures,2002(58):237-247. |
[4] | Luca Lanzi;Chiara Bizagni.Minimum weight optimization of composite stiffened panels u sin g neural networks[J].AIAA Journal,2003 |
[5] | W Liu;R Buffer;A.R Mileham;A J Green.Optimum design,experimental testing and post-buckling analysis of thick composite stiffened panels[J].A1AA Journal,2005 |
[6] | W Liu;R Buffer.Optimum buckling design of composite wing cover panels with manufacturing constraints[J].AIAA Journal,2007:2215. |
[7] | M.Lillico;R Buffer;G.W.Hunt.Optimum design and testing a post-buckled stiffened panel[J].AIAA Journal,2000:1659. |
[8] | R.Butler;F.W.Williams .Optimum design u sin g Ⅵ-CONOPT,a buckling and strength constraint program for prismatic assemblies of anisotropic plates[J].Computers & Structures,1992,43(04):699-708. |
[9] | 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(04):308-311,315. |
[10] | 李烁,徐元铭,张俊.基于神经网络响应面的复合材料结构优化设计[J].复合材料学报,2005(05):134-140. |
[11] | 卢险峰.最优化方法应用基础[M].上海:同济大学出版社,2003 |
[12] | 周明;孙树栋.遗传算法原理及应用[M].北京:国防工业出版社,1999 |
[13] | 王小平;曹立明.遗传算法-理论应用及软件实现[M].西安:西安交通大学出版社,2002 |
[14] | 雷英杰;张善文;李续武;周创明.Matlab遗传算法工具箱及应用[M].西安:西安电子科技大学出版社,2005 |
上一张
下一张
上一张
下一张
计量
- 下载量()
- 访问量()
文章评分
- 您的评分:
-
10%
-
20%
-
30%
-
40%
-
50%