Numerical Analysis of a Propellant Tank Slosh Baffle
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A current problem that severely affects the performance of spacecraft is related to slosh dynamics in liquid propellant tanks under microgravity conditions. Accurate prediction of the slosh dynamics is critical for successful mission planning and may impact vehicle control and positioning during rendezvous, docking, and reorientation maneuvers. The purpose of this work is to assess the performance of various slosh-mitigating baffle designs and configurations using computational fluid dynamics. This work develops metrics, including wall wetting, peak slosh amplitude, and bulk fluid motion, to assess the relevance of a particular baffle geometry and placement within the tank for a prescribed bulk fluid motion over a range of acceleration levels. The two- and three-dimensional studies are used to assess the slosh model’s sensitivity to grid resolution, laminar versus turbulent flow models, and Bond number scaling. The results are used to develop a foundation on which to build a full six-degree-of-freedom dynamic mesh model, allowing for fluid-force interaction with a propellant tank, which will be benchmarked against low-gravity slosh flight data.
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Vreeburg, J. P. B.: "Spacecraft Maneuvers and Slosh Control, IEEE Control Systems Magazine, June 2005.
Vreeburg, Jan P.B. and Chato, David, "Models for Liquid Impact Onboard Sloshsat FLEVO", NASA Technical Report NASA/TM—2000-210475, November 2000.
Ibrahim, R., A., Liquid Sloshing Dynamics: Theory and Applications. Cambridge University Press, © 2005.
Dodge, F. T. et al.: "The new dynamic behavior of liquids in moving containers", Technical Report, Southwest Research Institute, San Antonio, TX, 2000.
Dodge, F. T.: "Engineering study of flexible baffles for slosh suppression", NASA TR, Sep. 1, 1971.
Dodge, F. T.; Garza, L. R.: "Simulated low-gravity sloshing in spherical tanks and cylindrical tanks with inverted ellipsoidal bottoms", NASA Technical Report, Feb. 1, 1968
Schlee,K., Gangadharan, S., Ristow, J., Sudermann,J., Walker, C., Hubert, C.: "Modeling and Parameter Estimation of Spacecraft Fuel Slosh Mode", Proc. 2005 Winter Simulation Conference.
Abramson, H. N., et. al., Some studies of nonlinear lateral sloshing in rigid containers. NASA-CR-375, 1966.
Babskii, V. G., et. al., Hydromechanics of weightlessness. Izdatel'stvo Nauka , 504, 1976.
Narimanov, G. S., Koruchaev, L. V., & Lukovskii, I. A. (1977). Nonlinear dynamics of liquid-containing flight vehicles. Moscow: Izdatel'stvo Mashinostroenie.
Abramson, H. N., The Dynamic Behavior of Liquids in Moving Containers," NASA-SP-106, 1966.
Grayson, G. et. al., "Cryogenic Tank Modeling for the Saturn AS-203 Experiment", 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference, 9-12 July 2006.
Lamb, H., Hydrodynamics, Cambridge University Press, Cambridge, 7th ed., 1945.
Luppes, R., Helder, J. A. and Veldman, A.E.P.: "The Numerical Simulation Of Liquid Sloshing In Microgravity", European Conference on Computational Fluid Dynamics, Delft, The Netherlands, 2006.
Miles, J. W., On the Sloshing of Liquid in a Cylindrical Tank," Tech. Rep. GM-TR-18, The Ramo-Woolridge Corp. Guided Missile Research Div., April 1956.
Veldman, A.E.P.: "The Simulation of Violent Free-Surface Dynamics At Sea And In Space", European Conference on Computational Fluid Dynamics, Delft, The Netherlands, 2006.
Best practices for the VOF Model. Ansys., 2006.
Rhee, S. H., “Unstructured Grid Based Reynolds-Averaged Navier-Stokes Method for Liquid Tank Sloshing,” Journal of Fluids of Engineering, Vol. 127, May 2005, p. 572-582.
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