Rj. Hung et Hl. Pan, DIFFERENCES IN GRAVITY GRADIENT AND GRAVITY JITTER-EXCITED SLOSH WAVES IN MICROGRAVITY, Transactions of the Japan Society for Aeronautical and Space Sciences, 36(113), 1993, pp. 153-169
The dynamical behavior of fluids affected by the asymmetric gravity gr
adient acceleration and gravity jitter acceleration, in particular the
effect of surface tension on partially-filled rotating fluids applica
ble to a full-scale Gravity Probe-B Spacecraft dewar tank have been in
vestigated. Results of slosh wave excitation along the liquid-vapor in
terface induced by gravity gradient acceleration indicated that the gr
avity gradient acceleration is equivalent to the combined effect of a
twisting force and torsional moment acted on the spacecraft. The resul
ts are clearly seen from one-up one-down and one-down one-up oscillati
ons of two bubbles in the cross-section of profiles in the vertical r-
z plane of rotating dewar, and an eccentric contour of the bubble rota
ting around the axis of the dewar in a horizontal r-theta plane. Resul
ts of the slosh wave excitation along the liquid-vapor interface induc
ed by gravity jitter acceleration indicate that the gravity jitter acc
eleration is equivalent to time-dependent oscillatory forces which pus
h the bubble in the combined directions of down-and-up and sideward-an
d-middleward as the bubble is rotating with respect to rotating dewar
axis. Results also show that lower frequency gravity jitter accelerati
ons with turn-around directions imposed on the spacecraft container in
duce a greater amplitude of oscillations and a stronger degree of asym
metry in the liquid-vapor interface geometry than that made by the hig
her frequency gravity jitter acceleration. This study discloses the di
fferences in slosh wave excitation along the liquid-vapor interface dr
iven by gravity gradient acceleration and gravity jitter acceleration
which are two major driving forces affecting the stability of the flui
d system in microgravity.