Parametric resonance of liquid sloshing in partially filled spacecraft tanks during the powered-flight phase of rocket-Reference-Cited by-同舟云学术

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Parametric resonance of liquid sloshing in partially filled spacecraft tanks during the powered-flight phase of rocket

Published:2014-05 Issue: Volume:35 Page:93-105
ISSN:1270-9638
Container-title:Aerospace Science and Technology
language:en
Short-container-title:Aerospace Science and Technology

Author:

Cui De-Lin,Yan Shao-Ze,Guo Xiao-Song,Gao Robert X.

Funder

National Science Foundation of China

Scientific Research Foundation for the Returned Overseas Chinese Scholars

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference35 articles.

1. A numerical study of the effects of the vertical baffle on liquid sloshing in two-dimensional rectangular tank;Akyildiz;J. Sound Vib.,2012

2. Oscillations of a viscous liquid in a cylindrical container;Bauer;Aerosp. Sci. Technol.,1997

3. Free oscillations and response of a viscous liquid in a rigid circular cylindrical tank;Bauer;Aerosp. Sci. Technol.,1999

4. Frictionless liquid sloshing in circular cylindrical container configurations;Bauer;Aerosp. Sci. Technol.,1999

5. The New “Dynamic Behavior of Liquids in Moving Containers”;Dodge,2000

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