穆小强, 陈祖奎. 竖管-叶片式表面张力管理装置的设计与分析.火箭推进, 2013, 39(1): 15-18 (Mu Xiaoqiang, Chen Zukui. Design and analysis for standpipe and its vane surface tension management device. Journal of Rocket Propulsion, 2013, 39(1): 15-18 (in Chinese))
[2]
李永, 潘海林, 魏延明.第二代表面张力贮箱的研究与应用进展.宇航学报, 2007, 28(2): 503-507 (Li Yong, Pan Hailin, Wei Yanming. The evolvement of the study and application on the second generation surface tension tank. Journal of Astronautics, 2007, 28(2): 503-507 (in Chinese))
[3]
Tam W, Ballinger I, Jaekle, Jr. D E. Tank trade studies-an overview. AIAA2008-4940
[4]
Tam W H, Taylor J R. Design and manufacture of a repellant tank assembly. AIAA97-2813
[5]
Tam WH, Drey MD, Larsson LW. Design and manufacture of an oxidizer tank assembly. AIAA2001-3825
[6]
Debreceni MJ, Lay WD, Jaekle, Jr. D E. Design and development of a pmd-type bipropellant tank. AIAA 98-3200
[7]
Debreceni MJ, Uo TK, Jaekle, Jr. D E. Development of a titanium propellant tank. AIAA 2003-4604
[8]
Mclean C, Deininger W, Ingram K, et al. Mission demonstration concept for the long-duration storage and transfer of cryogenic propellants. IEEE Aerospace Conference, 2013. 1-11
[9]
魏延明, 潘海林.全管理圆柱形表面张力贮箱的微重力实验验证-静平衡与重定位. 控制工程, 1997, (5): 14-19 (Wei Yanming, Pan Hailing. The microgravity experiment of cylindrical surface tension tank - static equilibrium and reorientation. Control Engineering of China, 1997, (5): 14-19 (in Chinese))
[10]
李章国, 刘秋生, 纪岩等.航天器贮箱气液自由界面追踪数值模拟.空间科学学报, 2008, 28(1): 69-73 (Li Zhangguo, Liu Qiusheng, Ji Yan, et al. Numerical simulation of liquid-vapor interface tracking in tank of spacecraft. Chin J Space Sci , 2008, 28(1): 69-73 (in Chinese))
[11]
李京浩, 陈小前, 黄奕勇.基于内角流动的板式表面张力贮箱内推进剂流动过程研究.国防科技大学学报, 2012, 34(4): 21-24 (Li Jinghao, Chen Xiaoqian, Huang Yiyong. A study of propellant flow in the vane-type surface tension tank based on interior corner flow. Journal of National University of Defense Technology, 2012, 34(4): 21-24 (in Chinese))
[12]
胡齐, 李永, 耿永兵等.一种板式推进剂管理装置(Pmd)性能的数值仿真.空间控制技术与应用, 2010, 36(3): 59-62 (Hu Qi, Li Yong, Geng Yongbin, et al. Numerical Simulation for Capability of a Vane PMD to Manage Propellant. Aerospace Control and Application, 2010, 36(3): 59-62 (in Chinese))
[13]
胡齐, 李永, 潘海林等.微重力环境下大叶片板式贮箱内流体行为的数值仿真与试验验证.空间控制技术与应用, 2013, 39(2): 62-66 (Hu Qi, Li Yong, Pan Hailin, et al. Numerical simulation and experiment verification of fluid behavior in the vane type tank with big vanes in microgravity environment. Aerospace Control and Application, 2013, 39(2): 62-66 (in Chinese))
[14]
Concus P, Finn R, Weislogel M. Measurement of critical contact angle in a microgravity space experiment. Experiments in Fluids, 2000, 28: 197-205
[15]
张晨辉, 芮伟, 段俐等.基于板式表面张力的落塔实验.第九届全国实验流体力学学术会议论文. 2013: 278-282 (Zhang Chenhui, Rui Wei, Duan Li, et al. Falling tower experiment based on vane surface tension. In: Proc. the Ninth National Academic Conference on Experimental Fluid Mechanics. 2013: 278-282 (in Chinese))
[16]
Concus P, Finn R. On capillary free surfaces in a gravitational field. Acta Mathematica, 194, 132(1): 207-233
[17]
李京浩, 陈小前, 黄奕勇等.微重力环境下的不对称内角流动研究.中国科学: 技术科学, 2012, 42(8): 957-962 (Li Jinghao, Chen Xiaoqian, Huang Yiyong, et al. Study on asymmetric interior corner flow in microgravity condition. Sci China Tech Sci, 2012, 42(8): 957-962 (in Chinese))
[18]
刘玲, 李永强, 段俐等. 微重力下圆柱形不对称内角的毛细流动研究. 中国力学大会. 2013.
[19]
刘赵淼, 刘丽昆, 申峰. Y型微通道两相流内部流动特性.力学学报, 2014, 46(2): 209-216 (Liu Zhaomiao, Liu Likun, Shen Feng. Two-phase flow characteristics in Y-junction microchannel. Chinese Journal of Theoretical and Applied Mechanics , 2014, 46(2): 209-216 (in Chinese))
[20]
刘赵淼,刘佳,申峰. 不同重力下90o弯管内气液两相流流型及流动特性研究.力学学报, 2015, 47(2): 223-230 (Liu Zhaomiao, Liu Jia, Shen Feng. Simulation on flow patterns and characteristics of two-phase gas-liquid flow in a 90 bend under different gravity. Chinese Journal of Theoretical and Applied Mechanics, 2015, 47(2): 223-230 (in Chinese))
[21]
庄保堂, 李永, 潘海林等.微重力环境下导流叶片流体传输速度的试验研究.空间控制技术与应用. 2012, 38(6): 1-5 (Zhuang Baotang, Li Yong, Pan Hailin, et al. Experiment investigation on transportation velocity of the fluid on propellant acquisition vanes under microgravity environment. Aerospace Control and Application, 2012, 38(6): 1-5 (in Chinese))
