Dynamic Analysis of the Flexible Spacecraft with Liquid Sloshing in Axisymmetrical Container
Author:
Affiliation:
1. Beijing Institute of Technology, 100081 Beijing, People’s Republic of China
Funder
National Natural Science Foundation of China
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.A34005
Reference35 articles.
1. HastingsL. J.RutherfordR. “Low Gravity Liquid–Vapor Interface Shapes in Axisymmetric Containers and a Computer Solution,” NASA TM X-53790, 1968.
2. DodgeF. T. “The New ‘Dynamic Behavior of Liquids in Moving Containers’,” NASA SP-106, 2000.
3. Free and forced oscillations of a frictionless liquid in a long rectangular tank with structural obstructions at the free liquid surface
4. Hydroelastic vibrations in a two-dimensional rectangular container filled with frictionless liquid and a partly elastically covered free surface
5. Effects of Sloshing on Flutter Prediction of Liquid-Filled Circular Cylindrical Shell
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