微重力环境下充液航天器液体晃动动力学研究概述  

Introduction to Investigation of the Dynamics of Liquid Sloshing in Liquid-filled Spacecraft under Low Gravity Environment

作　　者：李云翔[1] 于益华[1] 

机构地区：[1]湖南城市学院数学与计算科学系,湖南益阳413049

出　　处：《湖南城市学院学报（自然科学版）》2005年第1期38-42,共5页Journal of Hunan City University:Natural Science

摘　　要：在充液航天器设计中有时需要考虑微重力环境下的液体晃动.微重力环境下的液体晃动问题比常重环境下复杂得多,很多问题有待深入研究.对微重力环境下液体晃动的解析研究方法作了简要介绍,并对其研究进展概要地进行了综述.Liquid sloshing under low gravity environment is a problem that must be considered during general design of liquid-filled spacecraft. Liquid sloshing under low gravity environment is much more complicated than under the normal gravity environment, so it’s essential to investigate it penetratingly. The analysis methods for studying liquid sloshing under low gravity environment are summarized and the advance of these problems is reviewed.

关 键 词：微重力环境 液体晃动 充液航天器 研究概述 动力学 航天器设计 研究方法 研究进展 

分 类 号：V524[航空宇航科学与技术—人机与环境工程] V414.1