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Slosh wave excitation in a partially filled rotating tank due to gravity jitters in a microgravity environmentThe 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.
Document ID
19930032003
Acquisition Source
Legacy CDMS
Document Type
Reprint (Version printed in journal)
Authors
Hung, R. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lee, C. C.
(Alabama Univ. Huntsville, United States)
Leslie, F. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1991
Publication Information
Publication: Acta Astronautica
Volume: 25
Issue: 9-Aug
ISSN: 0094-5765
Subject Category
Fluid Mechanics And Heat Transfer
Accession Number
93A16000
Funding Number(s)
CONTRACT_GRANT: NAG8-035
CONTRACT_GRANT: NAG8-128
Distribution Limits
Public
Copyright
Other

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