SLOSH WAVE EXCITATION IN A PARTIALLY FILLED ROTATING TANK DUE TO GRAVITY JITTERS IN A MICROGRAVITY ENVIRONMENT

被引：12

作者：

HUNG, RJ

LEE, CC

LESLIE, FW

机构：

[1] The University of Alabama in Huntsville, Huntsville

[2] NASA Marshall Space Flight Center, Huntsville

来源：

ACTA ASTRONAUTICA | 1991年 / 25卷 / 8-9期

关键词：

D O I：

10.1016/0094-5765(91)90035-4

中图分类号：

V [航空、航天];

学科分类号：

08 ; 0825 ;

摘要：

The dynamical behavior of fluids, in particular the effect of surface tension on partially-filled rotating fluids (cryogenic liquid helium and helium vapor), in a full-scale Gravity Probe-B Spacecraft propellant tank without probe imposed by various frequencies of gravity jitters have been investigated. Twelve case studies of slosh wave excitation due to various frequencies of gravity jitters under different rotating speeds of propellant tank and different levels of background gravity environment have been numerically simulated. Results disclose the conditions for the excitation of large amplitude slosh waves which shall be avoided in the design of cryogenic liquid propellant system.

引用

页码：523 / 551

页数：29

共 29 条

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