2018•Unpublished venueRequires access

Dynamic Characters of Liquid Sloshing in Partly-filled Spacecraft under Micro-gravity

Kecheng Lin, Xiaojuan Song, Yueying Ren, Hongwei Wang, Changjie Li

Abstract

Liquid propellant sloshing in partly-filled tank under micro-gravity is researched. Suppose the tank is rigid, ADINA and Fluent are used to analyze liquid sloshing in different-shape tanks under various fulfilling ratios and vibrating frequencies. The disciplines of each variable's change are summarized, and then common disciplines can be obtained and analyzed.

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Key concepts: Slosh dynamics, Adina, Spacecraft, Propellant, Fluent, Aerospace engineering, Physics, Mechanics