In the paper a review of the main problems in hypersonic aerothermodynamic- and aerodynamic research is presented. To develop useful design tools for re-entry vehicles a balanced combination of CFD codes (Computational Fluid Dynamics), wind tunnel experiments and free flight tests is needed. A flight test facility that fits into the present need can be simple and cost effective when flown as piggyback in the second stage of Ariane 4.


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    Titel :

    LARVE, a Hypersonic Flight Test Facility Launched by Ariane 4


    Beteiligte:
    R. Hagmeijer (Autor:in) / K. J. Sudmeijer (Autor:in)

    Erscheinungsdatum :

    1989


    Format / Umfang :

    21 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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