Current status of a steady state, axisymmetric analysis of an experimental 11 inch diameter hybrid rocket motor internal flow field is given. The objective of this effort is to develop a steady state axisymmetric model of the 11 inch hybrid rocket motor which can be used as a design and/or analytical tool. A test hardware description, modeling approach, and future plans are given. The analysis was performed with FDNS implementing several finite rate chemistry sets. A converged solution for a two equation and five species set on a 'fine' grid is shown.


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    Titel :

    Status of Axisymmetric CFD of an Eleven Inch Diameter Hybrid Rocket Motor


    Beteiligte:
    J. Ruf (Autor:in) / M. R. Sullivan (Autor:in) / T. S. Wang (Autor:in)

    Erscheinungsdatum :

    1993


    Format / Umfang :

    14 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch