Numerical Analysis of Sloshing and Wave Breaking in a Small Vessel by CIP-LSM(<Special Issue>CIP)

    • NONAKA Satoshi
    • Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency
    • NARUO Yoshihiro
    • Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency
    • INATANI Yoshifumi
    • Institute of Space and Astionautical Science, Japan Aerospace Exploration Agency

Abstract

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

JSME international journal. Ser. B, Fluids and thermal engineering   [List of Volumes]

JSME international journal. Ser. B, Fluids and thermal engineering 47(4), 709-715, 2004-11-15  [Table of Contents]

The Japan Society of Mechanical Engineers

References:  14

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Cited by:  4

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Codes

  • NII Article ID (NAID) :
    110004826639
  • NII NACSIS-CAT ID (NCID) :
    AA10888815
  • Text Lang :
    ENG
  • Article Type :
    Journal Article
  • ISSN :
    13408054
  • NDL Article ID :
    7149458
  • NDL Source Classification :
    ZN11(科学技術--機械工学・工業)
  • NDL Call No. :
    Z53-Y271
  • DOI :
    10.1299/jsmeb.47.709
  • Databases :
    CJP  CJPref  NDL  NII-ELS  J-STAGE