Stability analysis of liquid filled spacecraft system with flexible attachment by using the energy

Stability analysis of liquid filled spacecraft system with flexible attachment by using the energy–Casimir method

Published:2016-03 Issue:2 Volume:6 Page:100-106
ISSN:2095-0349
Container-title:Theoretical and Applied Mechanics Letters
language:en
Short-container-title:Theoretical and Applied Mechanics Letters

Author:

Yan Yulong,Yue Baozeng

Funder

National Natural Science Foundation of China

Innovation Fund Designated for Graduate Students of Beijing Institute of Technology

the Research Fund for the Doctoral Program of Higher Education of China

Publisher

Elsevier BV

Subject

Mechanical Engineering,Mechanics of Materials,Ocean Engineering,Aerospace Engineering,Biomedical Engineering,Civil and Structural Engineering,Environmental Engineering,Computational Mechanics

Reference31 articles.

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3. A mechanical model for low-gravity sloshing in an axisymmetric tank;Utsumi;Trans. ASME, J. Appl. Mech.,2004

4. An a priori estimate in the theory of hydrodynamic stability;Arnold;Izv. Vyssh. Uchebn. Zaved. Mat.,1966

5. Stability analysis of a rigid body with a flexible attachment using the energy–Casimir method;Posbergh;Commun. Contemp. Math.,1987

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