Without an adequate understanding of propellant slosh, the spacecraft attitude control system may be inadequate to control the spacecraft or there may be an unexpected loss of science observation time due to higher slosh settling times. Computational fluid dynamics (CFD) is used to model propellant slosh. STAR-CCM+ is a commercially available CFD code. This paper presents a comparison between STAR-CCM+ liquid slosh modeling results and experimental, empirically, and analytically derived results. The geometries examined are a bare right cylinder tank and a right cylinder


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    Titel :

    Validation of Slosh Modeling Approach Using STAR-CCM+


    Beteiligte:
    Benson, David (Autor:in) / Ng, Wanyi (Autor:in)

    Kongress:

    Space Propulsion 2018 ; 2018 ; Seville, Spain


    Erscheinungsdatum :

    18.05.2018


    Medientyp :

    Sonstige


    Format :

    Keine Angabe


    Sprache :

    Englisch