Modelling of sloshing modulated angular momentum fluctuations actuated by gravity gradient associated with spacecraft slew motion

DOI10.1016/0307-904X(95)00159-HzbMath0885.76007MaRDI QIDQ5961826

R. J. Hung, Hailin Pan

Publication date: 22 April 1998

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

zbMATH Keywords

stabilitymicrogravity environmentadvanced X-Ray Astrophysics Facility-Spectroscopy spacecraftcapillary effectcryogenic superfluid liquid helium IIDewar containernoninertial spacecraft-fitted coordinates

Mathematics Subject Classification ID

Statistical mechanics of superfluids (82D50) Jets and cavities, cavitation, free-streamline theory, water-entry problems, airfoil and hydrofoil theory, sloshing (76B10)

Cites Work

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