Volume 29 Issue 1
Jan.  2014
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ZHOU Suan, QIANG Hong-fu, WANG Xue-ren, WANG Guang, ZHOU Zhi-qing. Buckling load computation of spherical-cone diaphragms based on Kriging metamodel[J]. Journal of Aerospace Power, 2014, 29(1): 111-117. doi: 10.13224/j.cnki.jasp.2014.01.014
Citation: ZHOU Suan, QIANG Hong-fu, WANG Xue-ren, WANG Guang, ZHOU Zhi-qing. Buckling load computation of spherical-cone diaphragms based on Kriging metamodel[J]. Journal of Aerospace Power, 2014, 29(1): 111-117. doi: 10.13224/j.cnki.jasp.2014.01.014
shu

Buckling load computation of spherical-cone diaphragms based on Kriging metamodel

doi: 10.13224/j.cnki.jasp.2014.01.014
  • 1.

    Power Engineering Department, Xi'an Hi-Tech Institute, Xi'an 710025, China

  • 2.

    Survival Technology and Efficiency Assessment of Aerospacecraft Laboratory, Equipment Academy of the Second Artillery Force, Beijing 100085, China

  • Received Date: 2012-11-19
  • Publish Date: 2014-01-28
    Abstract
  • Regarding typical structural characteristics of radius and thickness of diaphragms,height and angle of cone section,a method was built to compute the buckling load of diaphragms based on Kriging metamodel.The Kriging metamodel was validated by typical samples.Research results show that:for the Kriging metamodel based on Cubic correlation function,the error percentage to compute buckling loads at untried inputs is less than 5%,more suitable for computing the buckling loads of spherical-cone diaphragms than that based on Gauss correlation function;the metamodel could precisely compute buckling loads at untried inputs,without need of modeling and simulation by finite element method;the metamodel could compute parameter values of typical structural characteristics according to a set buckling load,and also could be used as bound function or object function for structural optimization design of spherical-cone diaphragms.

     

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    • References(22)
  • [1]
    毛根旺, 唐金兰.航天器推进系统及其应用[M].西安:西北工业大学出版社, 2009.
    [2]
    Cardullo M W.Metal expulsion diaphragm development for spherical propellant tanks[R].NASA 62-666, 1962.
    [3]
    Stofan A J, Sumner I E.Experimental investigation of the slosh-damping effectiveness of positive-expulsion bags and diaphragms in spherical tanks[R].NASA TN D-1712, 1963.
    [4]
    Friona A J, Wood R.MX stage 4 propellant storage assembly.AD A103844, 1997.
    [5]
    何星星, 袁杰红, 周仕明.内环向加筋圆柱形金属膜片变形数值仿真与失效分析[J].强度与环境, 2007, 34(6):16-21. HE Xingxing, YUAN Jiehong, ZHOU Shiming.Deformation numerical simulation and failure analysis of ring-stiffened metal diaphragm for positive expulsion tanks[J].Structure and Environment Engineering, 2007, 34(6):16-21.(in Chinese)
    [6]
    张绪虎, 唐斌, 李金山, 等.航天器贮箱用钛制隔膜变形过程的数值模拟[J].宇航学报, 2010, 31(9):2184-2188. ZHANG Xuhu, TANG Bin, LI Jinshan, et al.Deformation numerical simulation of titanium diaphragm for spacecraft tank[J].Journal of Astronautics, 2010, 31(9):2184-2188.(in Chinese)
    [7]
    王刚.推进剂管理用金属膜片挤压变形有限元分析[D].哈尔滨:哈尔滨工业大学, 2009. WANG Gang.The finite element analysis of metal diaphragm deformation for propellant management device[D].Harbin:Harbin Institute of Technology, 2009.(in Chinese)
    [8]
    臧家亮.神州载人飞船推进分系统的研制[J].航天器工程, 2004, 13(1):57-64. ZANG Jialiang.The development of the propulsion subsystem of Shenzhou manned spaceship[J].Spacecraft Engineering, 2004, 13(1):57-64.(in Chinese)
    [9]
    强洪夫, 周算, 王广, 等.径厚比对锥柱形金属膜片屈曲和后屈曲状态的影响[J].航空动力学报, 2012, 27(11):2521-2528. QIANG Hongfu, ZHOU Suan, WANG Guang, et al.Effect of ratio of radius to thickness on buckling and post-buckling behaviors of metallic spherical-cone diaphragms for positive expulsion tanks[J].Journal of Aerospace Power, 2012, 27(11):2521-2528.(in Chinese)
    [10]
    Giunta A A.Aircraft multidisciplinary design optimization using design of experiments theory and response surface modeling methods[D].Blacksburg, US:Virginia Polytechnic Institute, 1997.
    [11]
    Simpson W, Mauery T M, Korte J J, et al.Comparison of response surface and linear models for multidisciplinary design optimization[R].AIAA 98-4755, 1998.
    [12]
    刘克龙, 姚卫星, 穆雪峰.基于Kriging代理模型的结构形状优化方法研究[J].计算力学学报, 2006, 23(3):344-347, 362. LIU Kelong, YAO Weixing, MU Xuefeng.A method of structural shape optimization based on Kriging model[J].Chinese Journal of Computational Mechanics, 2006, 23(3):344-347, 362.(in Chinese)
    [13]
    陈巍, 周雄辉, 张汝珍, 等.基于Kriging代理模型的注塑产品翘曲优化[J].上海交通大学学报, 2010, 44(4):588-592. CHEN Wei, ZHOU Xionghui, ZHANG Ruzhen, et al.Warpage optimization for injection molding based on Kriging metamodel[J].Journal of Shanghai Jiaotong University, 2010, 44(4):588-592.(in Chinese)
    [14]
    谢延敏, 徐笑梅, 罗征志.基于Kriging模型的翻边成形参数优化[J].塑性工程学报, 2010, 17(5):4-9. XIE Yanmin, XU Xiaomei, LUO Zhengzhi.Research on parameter optimization in flanging process based on Kriging metamodel[J].Journal of Plasticity Engineering, 2010, 17(5):4-9.(in Chinese)
    [15]
    刘纪涛, 刘飞, 张为华.Kriging模型在固体火箭发动机装药可靠性分析中的应用[J].航空动力学报, 2010, 25(1):193-197. LIU Jitao, LIU Fei, ZHANG Weihua.Application of Kriging model to reliability analysis of solid rocket motor grain[J].Journal of Aerospace Power, 2010, 25(1):193-197.(in Chinese)
    [16]
    韩永志, 高行山, 李立州, 等.基于Kriging模型的涡轮叶片多学科设计优化[J].航空动力学报, 2007, 22(7):1055-1059. HAN Yongzhi, GAO Hangshan, LI Lizhou, et al.Kriging model-based multidisciplinary design optimization for turbine blade[J].Journal of Aerospace Power, 2007, 22(7):1055-1059.(in Chinese)
    [17]
    陈志英, 任远, 白广忱, 等.粒子群优化的Kriging近似模型及其在可靠性分析中的应用[J].航空动力学报, 2011, 26(7):1522-1530. CHEN Zhiying, REN Yuan, BAI Guangchen, et al.Particle swarm optimized Kriging approximate model and its application to reliability analysis[J].Journal of Aerospace Power, 2011, 26(7):1522-1530.(in Chinese)
    [18]
    Sacks J, Welch W J, Mitchell T J, et al.Design and analysis of computer experiments[J].Statistical Science, 1989, 4(4):409-435.
    [19]
    Lophaven S N, Nielsen H B, Sndergaard J.DACE:a matlab Kriging toolbox[R].Informatics and Mathematical Modelling Report, IMM-REP-2002-12, 2002.
    [20]
    王琦.MDO优化算法研究[D].南京:南京航空航天大学, 2008. WANG Qi.Research on arithmetic of MDO[D].Nanjing:Nanjing University of Aeronautics and Astronautics, 2008.
    [21]
    嵇晓宇, 徐兵, 郁向东, 等.薄壳结构的非线性屈曲有限元分析[J].固体力学学报, 2003, 24(增刊):214-217. JI Xiaoyu, XU Bing, YU Xiangdong, et al.Finite element analysis of nonlinear buckling for thin shell[J].Acta Mechanica Solida Sinica, 2003, 24(suppl):214-217.(in Chinese)
    [22]
    黄克智.板壳理论[M].北京:清华大学出版社, 1987.
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