Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM

DOI Web Site Web Site 被引用文献5件 参考文献17件 オープンアクセス
  • HIMENO Takehiro
    Department of Aeronautics and Astronautics, University of Tokyo
  • WATANABE Toshinori
    Department of Aeronautics and Astronautics, University of Tokyo
  • NONAKA Satoshi
    Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
  • NARUO Yoshihiro
    Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency
  • INATANI Yoshifumi
    Institute of Space and Astronautical Science, Japan Aerospace Exploration Agency

この論文をさがす

説明

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.

収録刊行物

被引用文献 (5)*注記

もっと見る

参考文献 (17)*注記

もっと見る

キーワード

詳細情報 詳細情報について

問題の指摘

ページトップへ