By making two reasonable approximations a variation of sideslip rolling moment coefficient with load factor was obtained for an airplane. The first approximation is to replace the wing normal load factor by the airplane normal load factor; the second is to assume the wing deflection mode to be parabolic.


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    Title :

    A Simplified Expression for the Dihedral Effect of a Flexible Wing


    Contributors:

    Publication date :

    1955


    Size :

    2 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English




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