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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    Title :

    Hypersonic Stability Derivatives of Blunted Slender Cones


    Contributors:
    O. Walchner (author) / J. T. Clay (author)

    Publication date :

    1964


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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