Dynamic Characters of Liquid Sloshing in Partly-filled Spacecraft under Micro-gravity

被引：0
|
作者：
Lin, Kecheng [1 ]
Song, Xiaojuan [1 ]
Ren, Yueying [1 ]
Wang, Hongwei [1 ]
Li, Changjie [1 ]
机构：
[1] Inner Mongolia Univ Technol, Coll Mech Engn, Hohhot, Peoples R China
来源：
PROCEEDINGS OF 2018 INTERNATIONAL CONFERENCE ON INFORMATION SYSTEMS AND COMPUTER AIDED EDUCATION (ICISCAE 2018) | 2018年
基金：
中国国家自然科学基金;
关键词：
liquid-sloshing; propellant; tank; FEM;
D O I：
暂无
中图分类号：
TP [自动化技术、计算机技术];
学科分类号：
0812 ;
摘要：
Liquid propellant sloshing in partly-filled tank under micro-gravity is researched. Suppose the tank is rigid, ADINA and Fluent are used to analyze liquid sloshing in different-shape tanks under various fulfilling ratios and vibrating frequencies. The disciplines of each variable's change are summarized, and then common disciplines can be obtained and analyzed.
引用
收藏
页码：389 / 393
页数：5
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