A CFD Approach to Modeling Spacecraft Fuel Slosh
Author:
Affiliation:
1. Embry-Riddle Aeronautical University
2. NASA Launch Services Program
3. Orbital Sciences Corporation
Publisher
American Institute of Aeronautics and Astronautics
Link
http://arc.aiaa.org/doi/pdf/10.2514/6.2009-366
Reference7 articles.
1. Liquid motions in nonaxisymmetric, partially filled containers rotating at zero gravity
2. Schlee, K. Gangadharan, S.N., Ristow, J., Advanced Method to Estimate Fuel Slosh SimulationParameters,41stAIAAJointPropulsionConference,2005.
3. FLUENTSoftware Version 6.2.16,©2004FluentInc.
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