The roll-damping derivative is one of the many aerodynamic coefficients that influence the flight dynamics of a rolling missile. At present, the knowledge of this derivative is limited, especially for unfinned bodies of revolution in hypersonic flight. This note presents a quick method of approximating the hypersonic roll-damping derivative of a slight blunted cone. (Author)


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    Titel :

    Blunt-Cone Roll-Damping Derivative


    Beteiligte:
    B. Quinn (Autor:in)

    Erscheinungsdatum :

    1968


    Format / Umfang :

    7 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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