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Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM
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- HIMENO Takehiro
- Department of Aeronautics and Astronautics, University of Tokyo
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- WATANABE Toshinori
- Department of Aeronautics and Astronautics, University of Tokyo
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- NONAKA Satoshi
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- NARUO Yoshihiro
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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- INATANI Yoshifumi
- Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
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Description
For the prediction of sloshing in the propellant tank of a rocket vehicle, the preliminary investigation was conducted. The flow field in the propellant tank during the ballistic flight of the vehicle was experimentally reproduced with the sub-scale model. The lateral acceleration as large as about 0.8G was provided with a mechanical exciter and the deformation of the liquid surface in the small vessel was visualized with a high-speed camera. The sloshing phenomena were also simulated with the CFD code, called CIP-LSM. The important features of surface deformation and wave breaking were successfully reproduced in the computation.
Journal
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- JSME International Journal Series B
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JSME International Journal Series B 47 (4), 709-715, 2004
The Japan Society of Mechanical Engineers
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Details 詳細情報について
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- CRID
- 1390282679652685568
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- NII Article ID
- 110004826639
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- NII Book ID
- AA10888815
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- ISSN
- 13475371
- 13408054
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- NDL BIB ID
- 7149458
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- Text Lang
- en
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- Data Source
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- JaLC
- NDL Search
- Crossref
- CiNii Articles
- OpenAIRE
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- Abstract License Flag
- Disallowed