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全失重液体晃动的固有频率 被引量:3

NATURAL FREQUENCIES OF LIQUID SLOSH IN ZERO-GRAVITY VONDITION
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摘要 本文研究全失重条件下液滴、带核液体和球腔内液体晃动的固有频率,对于几何球对称系统,本文给出了其解析解;而对于非球对称系统,则采用边界元方法计算得到晃动频率的数值解。 The natural frequencies of a liquid drop, a liquid around a rigid center core and a liquid in a spherical tank have been investigated in the present paper. For the spherical systems, the analytical solution is given, while for the nonspherical systems, a boundary element method was adopted to solve the problems numerically.
作者 包光伟
出处 《宇航学报》 EI CSCD 北大核心 1994年第4期65-70,共6页 Journal of Astronautics
基金 国家自然科学基金
关键词 液滴动力学 液体晃动 边界元法 航天器 Drop-dynamics Liquid slosh Boundary element method
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参考文献4

  • 1包光伟,多体系动力学.理论、计算方法和应用,1992年
  • 2王照林,力学进展,1988年,18卷,3期,301页
  • 3王竹溪,特殊函数概论,1979年
  • 4Chu W H,Trans ASME J Appl Mech,1970年,37卷,828页

同被引文献18

  • 1陈健,范晴云.贮箱内推进剂微重力下晃动的有限元模拟及试验[J].上海航天,2004,21(3):15-19. 被引量:4
  • 2包光伟,刘延柱.三轴定向充液卫星的姿态稳定性[J].空间科学学报,1993,13(1):31-38. 被引量:17
  • 3YUE Baozeng,WANG Zhaolin.Nonlinear phenomena of three-dimensional liquid sloshing in microgravity environment[J].Chinese Science Bulletin,2006,51(20):2425-2431. 被引量:16
  • 4夏恒新,宝音贺西,郑亚.多腔充液晃动的等效特性[J].动力学与控制学报,2007,5(4):346-349. 被引量:5
  • 5HUNG R J, PAN H L, LEE C C, et al. Effect of asym-metric gravity jitter excited slosh waves at liquid-vapor interface under microgravity [C]//AIAA Materials Spe-cialist Conference-Coating Technology for Aerospace Systems. Washington D.C.:AIAA,1992:1-12.
  • 6DODGE F T. The new "dynamic behavior of liquids in moving containers" [M]. San Antonio:Southwest Re-search Institute, 2000:65-66.
  • 7ABRAMSON H N. The dynamic behavior of liquids in moving containers, with applications to space vehicle technology[M]. San Antonio:Southwest Research Insti-tute, 1966:387-388.
  • 8VERGALLA M, GARRY L, KIRK D, et al. Experi-mental and numerical investigation of reduced gravity fluid slosh dynamics[C]//The 44th AIAA/ASME/SAE/ ASEE Joint Propulsion Conference and Exhibit. Wash-ington D. C.:AIAA, 2008:4667.
  • 9YANG H Q, PURANDARE R, PEUGEOT J, et al. Prediction of liquid slosh damping using a high resolu-tion CFD tool[C]//The 48th AIAA/ASME/SAE/ASEE Joint Propulsion Conference and Exhibit. Washington D. C.:AIAA, 2012.
  • 10CHINTALAPATI S, KIRK D R. Parametric study of a propellant tank slosh baffle [C]//The 44th AIAA/ ASME/SAE/ASEE Joint Propulsion Conference and Ex-hibit. Washington D. C.:AIAA, 2008.

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