@inproceedings{9181ac6051474343999db709e3b30713,
title = "The equivalent mechanical model for spacecraft for solving spacecraft large amplitude liquid sloshing problem",
abstract = "The development of vehicle capability brings growing command on large liquid tank. The disturbance brought by the liquid sloshing that generated in this kind of large liquid tank plays a non-negligible role to the spacecraft. In this paper, we illustrate a changing structure liquid sloshing probability model based on fluid dynamics under microgravity state, and use it as an equivalent model for large amplitude liquid sloshing. The results prove the accuracy of this method by comparing it with the result of CFD method. This proposed equivalent dynamic model take less time to solve to the theoretical method and also requires less storage versus computational fluid dynamics, due to its lower complexity.",
author = "Shiping Xing and Zhanxia Zhu and Jianping Yuan and Zhengyang Mao",
year = "2015",
language = "英语",
series = "Proceedings of the International Astronautical Congress, IAC",
publisher = "International Astronautical Federation, IAF",
pages = "6122--6127",
booktitle = "66th International Astronautical Congress 2015, IAC 2015",
note = "66th International Astronautical Congress 2015: Space - The Gateway for Mankind's Future, IAC 2015 ; Conference date: 12-10-2015 Through 16-10-2015",
}