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Effect of asymmetric gravity jitter excited slosh waves at liquid-vapor interface under microgravityThe dynamical behavior of fluids affected by the asymmetric gravity jitter oscillations, in particular the effect of surface tension on partially-filled rotating fluids (cryogenic liquid helium and helium vapor) in a sub-scale Gravity Probe-B Spacecraft propellant dewar tank imposed by time-dependent various directions of background gravity environment have been investigated. Results show that lower frequency gravity jitter imposed on the time-dependent variations of the direction of background gravity induced a greater amplitude of oscillations and a stronger degree of asymmetry in liquid-vapor interface geometry than that made by the higher frequency gravity jitter. Furthermore, the greater the components of background gravity in radial and circumferential directions will provide a greater contribution in driving more to the increasing amplitude and degrees of symmetry of liquid-vapor interface profiles which, in turn, modify the disturbance of moment of inertia and angular momentum of spacecraft.
Document ID
19920043082
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Hung, R. J.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Pan, H. L.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Lee, C. C.
(Alabama, University Huntsville, United States)
Leslie, F. W.
(NASA Marshall Space Flight Center Huntsville, AL, United States)
Date Acquired
August 15, 2013
Publication Date
January 1, 1992
Subject Category
Fluid Mechanics And Heat Transfer
Report/Patent Number
AIAA PAPER 92-0247
Accession Number
92A25706
Funding Number(s)
CONTRACT_GRANT: NAG8-129
CONTRACT_GRANT: NAG8-035
Distribution Limits
Public
Copyright
Other

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