Volume 42 Issue 4
Jul.  2012
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LI Qing, WANG Tianshu, MA Xingrui. REVIEWS ON LIQUID SLOSHING DYNAMICS AND LIQUID-STRUCTURE COUPLING DYNAMICS IN LIQUID-FILLED SPACECRAFTS[J]. Advances in Mechanics, 2012, 42(4): 472-481. doi: 10.6052/1000-0992-12-019
Citation: LI Qing, WANG Tianshu, MA Xingrui. REVIEWS ON LIQUID SLOSHING DYNAMICS AND LIQUID-STRUCTURE COUPLING DYNAMICS IN LIQUID-FILLED SPACECRAFTS[J]. Advances in Mechanics, 2012, 42(4): 472-481. doi: 10.6052/1000-0992-12-019

REVIEWS ON LIQUID SLOSHING DYNAMICS AND LIQUID-STRUCTURE COUPLING DYNAMICS IN LIQUID-FILLED SPACECRAFTS

doi: 10.6052/1000-0992-12-019
Funds:  The project was supported by the National Natural Science Foundation of China (11172145).
More Information
  • Corresponding author: MA Xingrui
  • Received Date: 2011-02-27
  • Rev Recd Date: 2012-07-03
  • Publish Date: 2012-07-25
  • As the capacity of launch vehicles, the lifespan of satellites and the complexity of deep space missions increase, the mass proportions of liquid propellant in spacecrafts are enhanced accordingly. Sloshing of liquid propellant in spacecrafts might affect the motion stability and the attitude and orbit control system, which is of particular concern in spacecraft dynamics. The sloshing liquid in a liquid-filled spacecraft is a distributed parameter system which is theoretically infinite dimensional, however, a simplified and reduced model is preferred in engineering. Therefore, equivalent mechanical models for liquid sloshing are continually studied. Moreover, the fluid-structure interaction between liquid propellant and tanks has important effects on the structural dynamics of spacecrafts, which is also of concern in liquid-filled spacecraft dynamics. First in this paper, the liquid sloshing studies are respectively reviewed regarding theoretical researches, numerical studies, experimental investigations and equivalent mechanical models. Then the numerical methods and application programs in fluid-structural interaction modeling are summarized. Finally, further research directions are suggested based on the development needs of spacecraft engineering.

     

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