Liquid-vapor Interface Configuration of the Axis-symmetrical Tanks with Curved Walls
The propellant sloshing behavior in spacecraft liquid container plays a vital role in the dynamical analysis and overall design of spacecraft, while the liquid-vapor interface configuration of liquid fuel in microgravity environment is the premise and basis of the study of liquid sloshing behavior....
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Veröffentlicht in: | Microgravity science and technology 2022-07, Vol.34 (4), Article 60 |
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creator | Yan, Yu-long Deng, Yue Song, Xiao-juan Deng, Ming-le Yue, Bao-zeng |
description | The propellant sloshing behavior in spacecraft liquid container plays a vital role in the dynamical analysis and overall design of spacecraft, while the liquid-vapor interface configuration of liquid fuel in microgravity environment is the premise and basis of the study of liquid sloshing behavior. The static liquid surface of axis-symmetric container was studied in this paper. The shape of liquid surface was characterized by using the polar coordinate system, and the nonlinear differential governing equation was derived. An appropriate algorithm was designed to numerically calculate the configuration of vapor-liquid interface configuration of the axis-symmetric containers, such as sphere, ellipsoid, and Cassini container. The rationality and effectiveness of the algorithm were verified by comparing the numerical results with the drop tower experimental data. Engineers and scholars could quickly and accurately acquire liquid-vapor interface configuration of the container by this technique. |
doi_str_mv | 10.1007/s12217-022-09984-x |
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The static liquid surface of axis-symmetric container was studied in this paper. The shape of liquid surface was characterized by using the polar coordinate system, and the nonlinear differential governing equation was derived. An appropriate algorithm was designed to numerically calculate the configuration of vapor-liquid interface configuration of the axis-symmetric containers, such as sphere, ellipsoid, and Cassini container. The rationality and effectiveness of the algorithm were verified by comparing the numerical results with the drop tower experimental data. 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subjects | Aerospace engineering Aerospace Technology and Astronautics Algorithms Boundary conditions Classical and Continuum Physics Configurations Contact angle Containers Coordinate systems Differential equations Drop towers Engineering Interfaces Liquid fuels Liquid sloshing Liquid surfaces Liquid-vapor interfaces Microgravity Multinational space ventures Original Article Polar coordinates Propellant tanks Space Exploration and Astronautics Space Sciences (including Extraterrestrial Physics Spacecraft Spacecraft design Working conditions |
title | Liquid-vapor Interface Configuration of the Axis-symmetrical Tanks with Curved Walls |
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