Mathematical model of bubble sloshing dynamics for cryogenic liquid helium in orbital spacecraft Dewar container

DOI10.1016/0307-904X(95)00033-GzbMath0833.76086WikidataQ126382829 ScholiaQ126382829MaRDI QIDQ1900586

R. J. Hung, Hailin Pan

Publication date: 11 March 1996

Published in: Applied Mathematical Modelling (Search for Journal in Brave)

zbMATH Keywords

capillary effectgravity gradientspinning motionadvanced \(X\)-ray astrophysics facility spectroscopygravity probe-Bjitter accelerationsmicrogravity liquid-vapor interfaceslew motion

Mathematics Subject Classification ID

Incompressible viscous fluids (76D99) General theory of rotating fluids (76U05) Orbital mechanics (70M20) General theory of mathematical modeling (00A71)

Related Items (3)

Sloshing of a layered fluid with a free surface as a Hamiltonian system ⋮ Modelling of sloshing modulated angular momentum fluctuations actuated by gravity gradient associated with spacecraft slew motion ⋮ Fully coupled interface-tracking model for axisymmetric ferrohydrodynamic flows

Cites Work

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• A calculation procedure for heat, mass and momentum transfer in three- dimensional parabolic flows
• Numerical Calculation of Time-Dependent Viscous Incompressible Flow of Fluid with Free Surface
• Spacecraft dynamical distribution of fluid stresses activated by gravity-jitter-induced slosh waves
• Asymmetric slosh wave excitation in a liquid-vapor interface under microgravity
• Sloshing dynamics-modulated fluid angular momentum and moment fluctuations driven by orbital gravity gradient and jitter accelerations in microgravity

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