CFD simulation of Pressure Drops in Liquid Acquisition Device Channel with Sub-Cooled Oxygen
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CFD simulation of Pressure Drops in Liquid Acquisition Device Channel with Sub-Cooled Oxygen

Authors: David J. Chato, John B. McQuillen, Brian J.Motil, David F. Chao, Nengli Zhang

Abstract:

In order to better understand the performance of screen channel liquid acquisition devices (LADs) in liquid oxygen (LOX), a computational fluid dynamics (CFD) simulation of LOX passing through a LAD screen channel was conducted. In the simulation, the screen is taken as a 'porous jump' where the pressure drop across the screen depends on the incoming velocity and is formulated by Δp = Av + Bv2 . The CFD simulation reveals the importance of the pressure losses due to the flow entering from across the screen and impacting and merging with the channel flow and the vortices in the channel to the cumulative flow resistance. In fact, both the flow resistance of flows impact and mergence and the resistance created by vortices are much larger than the friction and dynamic pressure losses in the channel and are comparable to the flow resistance across the screen. Therefore, these resistances in the channel must be considered as part of the evaluation for the LAD channel performance. For proper operation of a LAD in LOX these resistances must be less than the bubble point pressure for the screen channel in LOX. The simulation also presents the pressure and velocity distributions within the LAD screen channel, expanding the understanding of the fluid flow characteristics within the channel.

Keywords: Liquid acquisition devices, liquid oxygen, pressure drop, vortex, bubble point, flow rate limitation.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1085443

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[1] D. A. Fester, A. J. Villars, and P. E. Uney, "Surface tension propellant acquisition system technology for space shuttle reaction control tanks," J. Spacecraft, vol. 13, No.9, pp. 522-527, 1976,.
[2] M. T. Kudlac, J. M. Jurns, "Screen channel liquid acquisition devices for liquid oxygen," presented at the 42nd AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Sacramento, CA., July 9-12, 2006, Paper AIAA 2006-5054.
[3] M. V. Dyke, "Identification of influential factors for liquid acquisition device designs," presented at 34th Joint Propulsion Conference and Exhibit, Cleveland, OH, July 13-15, 1998, Paper AIAA-98-3198.
[4] D. J. Chato, and M. T. Kudlac, "Screen channel liquid acquisition devices for cryogenic propellants," presented at 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Indianapolis, IN., July 7-10, 2002, Paper AIAA 2002-3983.
[5] J. M. Jurns, and J. B. McQuillen, "Liquid acquisition device testing with sub-cooled liquid oxygen," presented at 44th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, Hartford, CT., July 21-23, 2008, Paper AIAA 2008-4943.
[6] J. C. Armour, and J. N. Cannon, "Fluid flow through woven screens," Journal AIChE, vol. 14, No. 3, pp. 415-420, 1968.
[7] E. C. Cady, "Study of thermodynamic vent and screen baffle integration for orbital storage and transfer of liquid hydrogen," NASA-cr-134482, August 1973.