Study on the coupled dynamics of rigid-liquid-flexible spacecraft by using isogeometric analysis for liquid sloshing

DOI10.1016/j.apm.2022.08.026zbMath1505.70055OpenAlexW4293382375MaRDI QIDQ2110830

Jiarui Yu, Bao-Zeng Yue

Publication date: 23 December 2022

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

Full work available at URL: https://doi.org/10.1016/j.apm.2022.08.026

zbMATH Keywords

level set methodisogeometric analysisliquid sloshing modelingrigid-liquid-flexible spacecraft

Mathematics Subject Classification ID

Variable mass, rockets (70P05) Mathematical modeling or simulation for problems pertaining to fluid mechanics (76-10)

Cites Work

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