A semiempirical theory is presented based on Cheng's analysis of slender blunted cones at zero angle of attack, while the tangent cone approximation is used to account for angle-of-attack effects. Quasi steady-state conditions are assumed to be valid.


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    Titel :

    Hypersonic Stability Derivatives of Blunted Slender Cones


    Beteiligte:
    O. Walchner (Autor:in) / J. T. Clay (Autor:in)

    Erscheinungsdatum :

    1964


    Format / Umfang :

    2 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch




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