Calculation study of wing-aileron flutter in two degrees of freedom for two-dimensional supersonic flow.


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    Title :

    Calculation study of wing-aileron flutter in two degrees of freedom for two-dimensional supersonic flow


    Additional title:

    NACA -- Tech Note


    Contributors:
    Woolston, D.S. (author) / Huckel, V. (author)


    Publication date :

    1954


    Size :

    26 pages


    Type of media :

    Report


    Type of material :

    Print


    Language :

    English


    Keywords :


    A theoretical investigation on wing-aileron-tab flutter

    Frazer, R. A. / Jones, W. P. | TIBKAT | 1955


    Flutter prediction for a wing with active aileron control

    Penning, K. / Sandlin, D. R. | NTRS | 1983


    Flutter Prediction for a Wing with Active Aileron Control

    K. Penning / D. R. Sandlin | NTIS | 1983