Presented in this report are the results of an investigation to evaluate aerodynamically the use of very low aspect-ratio fins, capped fins and shrouded fins to provide flight stability for the hypervelocity air-to-ground rocket (HAGR) configuration. Static-stability data were obtained for the HAGR configurations at Mach numbers ranging from 0.9 to 7.71.


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    Titel :

    Preliminary Wind Tunnel Investigation of the HAGR Configurations at Transonic, Supersonic and Hypersonic Mach Numbers


    Beteiligte:
    C. A. Kalivretenos (Autor:in) / R. T. Hall (Autor:in)

    Erscheinungsdatum :

    1966


    Format / Umfang :

    58 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch