Study on Free-surface Flows in Aerospace Propulsion Systems
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概要
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For the establishment of the technology for the management of liquid propellant in space vehicles, a numerical method, called ‘CIP-LSM’ (CIP based Level Set method & MARS), was developed to simulate three-dimensional free-surface flows under various gravity conditions. The dynamic behaviors of liquid in the model tank with multiple ring-baffles were successfully simulated.
著者
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Watanabe Toshinori
Department Of Aeronautics And Astronautics The University Of Tokyo
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Himeno Takehiro
Department Of Aeronautics And Astronautics The University Of Tokyo
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Inoue Chihiro
Department Of Aeronautics And Astronautics The University Of Tokyo
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INOUE Chihiro
Department of Aeronautics and Astronautics, University of Tokyo
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Himeno Takehiro
Department of Aeronautics and Astronautics, University of Tokyo
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