BAFFLE EFFECT ON SLOSHING-MODULATED TORQUES RESPONSED TO ORBITAL ACCELERATIONS IN MICROGRAVITY

被引:3
作者
HUNG, RJ
PAN, HL
机构
[1] University of Alabama in Huntsville, Huntsville, AL
[2] Department of Mechanical and Aerospace Engineering, University of Alabama in Huntsville, Huntsville, AL
基金
美国国家航空航天局;
关键词
D O I
10.2514/3.26675
中图分类号
V [航空、航天];
学科分类号
08 ; 0825 ;
摘要
The behavior of sloshing-dynamics-modulated fluid systems driven by orbital accelerations including gravity gradient and jitter accelerations has been studied. Partly liquid-filled rotating Dewars applicable to a full-scale Gravity Probe-B Spacecraft container with and without baffle are considered. Results show that a slosh wave excited along the liquid-vapor interface induced by jitter-acceleration dominated orbital accelerations provides a torsional moment with an up-and down movement of bubble oscillations in the rotating Dewar. The fluctuations of fluid forces and fluid moment (torque) exerted on the Dewar wall of the container caused by slosh-wave excitation driven by orbital accelerations are also investigated. Since the viscous force across a liquid-solid interface and the surface-tension force across a liquid vapor or liquid-solid interface ran greatly contribute to the damping effect of slosh-wave excitation, a rotating Dewar with a baffle provides more areas of liquid-solid, and liquid-vapor, and solid-vapor interfaces than does a rotating Dewar without a baffle, Results show that the damping effect provided by the baffle reduces the amplitudes of force and moment feedback from the fluids to the container-in particular, the components of fluctuations transverse to the direction of the baffle boards.
引用
收藏
页码:723 / 731
页数:9
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