Numerical Simulation of Liquid Oxygen and Gaseous Helium Separation under Microgravity Conditions
Authors: Kukshinov N.V., Evstigneeva V.E., Gantsev A.A., Podchufarov A.A.
Published in issue: #8(176)/2026
Category: Mechanics | Chapter: Mechanics of Liquid, Gas, and Plasma
The paper presents the results of numerical simulation of the separation process of liquid oxygen and gaseous helium under microgravity conditions in a spherical tank rotating about a transverse axis. The mathematical model is based on the Navier–Stokes equations for a two-phase incompressible fluid in a rotating reference frame. The volume of fluid (VOF) method in combination with the continuum surface force (CSF) model, which accounts for capillary effects and wall wetting, is used to track the interface. Turbulent characteristics are calculated using the two-equation k–ω SST turbulence model. A series of simulations was performed on successively refined unstructured polyhedral meshes (300k, 600k, and 1.5 million cells). A specialized clustering algorithm written in C was developed to automatically determine the separation time – the moment when more than 99% of the gas volume accumulates near the wall. It was found that insufficient spatial resolution leads to a simulation error in separation time of up to 20%. Transition from the intermediate mesh (600k cells) to the fine mesh (1.5 million cells) reduces the error to 7.7%. It is shown that the shift of the system’s center of mass along the X and Y axes reaches 6 mm and 5 mm, respectively, for a tank radius of 150 mm, and the projections of forces onto the walls reach a steady state after the completion of transient processes. The results are compared with data from the FLUIDICS space experiment.
EDN FNZZZO
References
[1] Bychkov A.D. Sposob dozapravki zhidkim toplivom kosmicheskogo ob"ekta v kosmicheskom prostranstve [Method for refueling a space object with liquid fuel in outer space]. Patent No. 2787259 Russian Federation, 2023, bull. no. 1, 6 p.
[2] Perfilyev L.A., Podobedov G.G., Sokolov B.A. Issledovanie voprosov gidromekhaniki v usloviyakh nevesomosti na bortu orbital’noy stantsii Mir [Investigation of hydromechanics issues under weightlessness conditions aboard the Mir orbital station]. Izvestiya RAN. Mekhanika tverdogo tela — Mechanics of Solids, 2003, no. 4, pp. 44–50.
[3] Storey J.M., et al. Progress towards a microgravity CFD validation study using the ISS SPHERES-SLOSH experiment. AIAA Propulsion and Energy 2020 Forum. Reston, VA, AIAA, 2020, p. 3814.
[4] Lapilli G. Design of a liquid sloshing experiment to operate in the International Space Station. 51st AIAA/SAE/ASEE Joint Propulsion Conference. Reston, VA, AIAA, 2015, p. 4074.
[5] Abramson H.N. The dynamic behavior of liquids in moving containers, with applications to space vehicle technology. NASA SP-106. Washington, D.C., NASA, 1967.
[6] Konopka M., Behruzi P., Schmitt S., Dreyer M. Phase change in cryogenic upper stage tanks. 50th AIAA/ASME/SAE/ASEE Joint Propulsion Conference. Reston, VA, AIAA, 2014, AIAA 2014-3998.
[7] von Rüden D. Pressurization behavior of a cryogenic propellant tank in microgravity. Master’s thesis. Bremen, Universität Bremen, 2021.
[8] Brackbill J.U., Kothe D.B., Zemach C. A continuum method for modeling surface tension. Journal of Computational Physics, 1992, vol. 100, no. 2, pp. 335–354.
[9] Hardy T.L., Tomsik T.M. Prediction of the ullage gas thermal stratification in a NASP vehicle propellant tank experimental simulation using FLOW-3D. NASA Technical Memorandum 103217. Washington, D.C., NASA, 1990.
[10] Wang L., Li Y., Li C., Zhao Z. CFD investigation of thermal and pressurization performance in LH2 tank during discharge. Cryogenics, 2013, vol. 57, pp. 63–73.
[11] Liu D., Lin P. A numerical study of three-dimensional liquid sloshing in tanks. Journal of Computational Physics, 2008, vol. 227, no. 8, pp. 3921–3939.
[12] Sussman M., Smereka P., Osher S. A level set approach for computing solutions to incompressible two-phase flow. Journal of Computational Physics, 1994, vol. 114, no. 1, pp. 146–159.
[13] Dalmont A., et al. Comparison between the FLUIDICS experiment and direct numerical simulations of fluid sloshing in spherical tanks under microgravity conditions. Microgravity Science and Technology, 2019, vol. 31, pp. 123–135.
[14] Green M.D., Zhou Y., Dominguez J.M., Gesteira M.G., Peiro J. Smooth particle hydrodynamics simulations of long-duration violent three-dimensional sloshing in tanks. Ocean Engineering, 2021, vol. 229, art. 108925.
[15] Trimulyono A., et al. Investigation of sloshing in the prismatic tank with vertical and T-shape baffles. Brodogradnja: An International Journal of Naval Architecture and Ocean Engineering for Research and Development, 2022, vol. 73, no. 2, pp. 43–58.
[16] Huang C.-Y., Wang J.-F., Zhao W.-W., Wan D.-C. Numerical simulation of liquid sloshing in a spherical tank by MPS method. Journal of Hydrodynamics, 2024, vol. 36, no. 2, pp. 232–240.
[17] Storey J.M., Kirk D.R. Experimental investigation of spherical tank slosh dynamics with water and liquid nitrogen. Journal of Spacecraft and Rockets, 2020, vol. 57, no. 5, pp. 876–890.
[18] Harvie D.J.E., Davidson M.R., Rudman M. An analysis of parasitic current generation in volume of fluid simulations. Applied Mathematical Modelling, 2006, vol. 30, no. 10, pp. 1056–1066.
[19] Heyns J.A., Oxtoby O.F. Modelling surface tension dominated multiphase flows using the VOF approach. 11th World Congress on Computational Mechanics (WCCM XI). Barcelona, 2014.
[20] Scheufler H., Roenby J. Accurate and efficient surface reconstruction from volume fraction data on general meshes. Journal of Computational Physics, 2019, vol. 383, pp. 1–23.
[21] Martinez J.M., Chesneau X., Zeghmati B. A new curvature technique calculation for surface tension contribution in PLIC-VOF method. Computational Mechanics, 2006, vol. 37, no. 2, pp. 182–193.