Box method for obtaining generalized air forces on oscillating wing in supersonic flow consists of representing wing by grid of square boxes and determining influence of one box on another; aerodynamic pressure influence coefficients when tabulated, permit flutter analysis of arbitrary wing with arbitrary normal modes to be carried out in routine way.


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    Title :

    Aerodynamic flutter derivatives for flexible wing with supersonic and subsonic edges


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Pines, S. (author) / Dugundji, J. (author) / Neuringer, J. (author)

    Published in:

    Publication date :

    1955


    Size :

    8 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :