Validated spherical pendulum model for rotary liquid slosh
Author:
Affiliation:
1. Southwest Research Institute, San Antonio, Texas
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/3.26052
Reference5 articles.
1. Digital data analysis techniques for extraction of slosh model parameters
2. A model for nonlinear rotary slosh in propellant tanks
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