[1] Friona AJ, Wood R. MX stage4 propellant storage assembly. AD A103844: 97-111
[2]
[2] 王刚. 推进剂管理用金属膜片挤压变形有限元分析. 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. Harbin: Harbin Institute of Technology, 2009 (in Chinese))
[3]
[3] 周仕明, 袁杰红. 金属膜片贮箱膜片变形的数值模拟与失效分析. 上海航天, 2005 (6): 13-16,54 (Zhou Shiming, Yuan Jiehong. Deformation numerical simulation and failure analysis of metal diaphragm for positive expulsion tanks. Aerospace Shanghai, 2005 (6): 13-16,54 (in Chinese))
[4]
[4] 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. 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. Journal of Astronautics, 2010, 31(9): 2184-2188 (in Chinese))
[5]
[5] 张增亭. 金属膜片贮箱膜片的数值仿真与试验验证. 火箭推进, 2009, 35(3): 26-29 (Zhang Zengting. Numerical simulation and test verification of diaphragm for metal diaphragm tank. Journal of Rocket Propulsion, 2009, 35(3): 26-29 (in Chinese))
[6]
[6] 朱志华, 胡小平, 陈香林. 钛制金属贮箱膜片的有限元分析. 火箭推进, 2007, 33(4): 32-35,51 (Zhu Zhihua, Hu Xiaoping, Chen Xianglin. Finite element analysis of the overturning process of titanium diaphragm for propellant tank. Journal of Rocket Propulsion, 2007, 33(4): 32-35,51 (in Chinese))
[7]
[7] 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. 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. Structure Environment Engineering, 2007, 34(6): 16-21 (in Chinese))
[8]
[8] 何星星, 周仕明, 袁杰红. 锥柱形加筋金属膜片变形的数值仿真分析. 火箭推进, 2007, 33(6): 34-37 (He Xingxing, Zhou Shiming, Yuan Jiehong. Deformation numerical simulation analysis of stiffened metal diaphragm for positive expulsion tank. Journal of Rocket Propulsion, 2007, 33(6): 34-37 (in Chinese))
[9]
[9] 《数学手册》编写组. 数学手册. 北京: 高等教育出版社, 1977
[10]
[10] 汪荣鑫. 数理统计. 西安: 西安交通大学出版社, 1986
[11]
[11] 赵桂平, 赵锺斗. 基于改进弧长法的层压复合壳后屈曲反应分析. 工程力学, 2003, 20(1): 106-111(Zhao Guiping, Cho Chongdu. Postbuckling analysis of laminated composite shell based on an improved arc-length method. Engineering Mechanics, 2003, 20(1): 106-111 (in Chinese))
