Sloshing-Modulated Liquid-Vapor Interface Fluctuations Activated by Orbital Accelerations Associated with Spinning and/or Slew Motions

• Published in: Journal of colloid and interface science Vol. 170; no. 2; pp. 538 - 549
• Main Authors: Hung, R.J., Pan, H.L.
• Format: Journal Article
• Language: English
• Published: San Diego, CA Elsevier Inc 15.03.1995; Elsevier
• Subjects: Acceleration; Boundary conditions; Computational methods in fluid dynamics; Dewars; Drag; Exact sciences and technology; Fluid dynamics; Fundamental areas of phenomenology (including applications); Gravitation; Hydrodynamic stability; Interfacial instability; Machine vibrations; Oscillations; Partial differential equations; Physics; Spacecraft; Superfluid helium; Three dimensional; Fluid dynamics; Liquid vapor interface; Spacecraft; Superfluid; Theoretical study; Gravity acceleration; Mathematical models; Application
• ISSN: 0021-9797; 1095-7103
• DOI: 10.1006/jcis.1995.1132

The formulation of sloshing dynamics for a Dewar partially filled with cryogenic superfluid helium II driven by both gravity gradient and jitter accelerations associated with spinning and/or slew motions in a microgravity environment is investigated. The jitter accelerations include slew motion, spinning motion, atmospheric drag on the spacecraft, spacecraft attitude motions arising from machinery vibrations, thruster firing, pointing control of spacecraft, and crew motion. The numerical computation of sloshing dynamics is carried out through the formulation of noninertial frame spacecraft-bound coordinates and the solution of three-dimensional formulations of time-dependent, partial differential equations subject to initial and boundary conditions. The examples given demonstrate how sloshing dynamics affects the liquid-vapor interface oscillations of cryogenic superfluid helium II driven by orbital accelerations of a spacecraft associated with spinning and/or slew motions.