Simplified vector method given for accurate determination of critical flutter speeds of oscillating airfoil flap system; solution of three-degree case is based on fact that components of vibratory determinant are complex in form (real part plus imaginary part) and therefore can be represented by vector in complex plant. Before Inst Aeronautical Sciences.


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    Title :

    Vector solution of three-degree case of wing bending, wing torsion, aileron flutter


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Arnold, L. (author)


    Publication date :

    1942


    Size :

    4 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :




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