Investigation formulates flutter problem of wing aileron tab combination with aerodynamic overhang in terms of system of six linear ordinary differential equations of motion with constant coefficients.


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    Title :

    Two-dimensional transient motion and flutter of wing having four degrees of freedom


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Reismann, H. (author) / Best, G.C. (author)


    Publication date :

    1952


    Size :

    3 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :