Study of relationship between node point location and inertia and elastic characteristics of airfoil, and particularly of characteristics that determine node at 3/4 chord point is made to provide information useful in designing so as to avoid flutter.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Influence of some parameters in flutter problem


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Isakson, G. (author) / O'Brien, T.F. (author)


    Publication date :

    1950


    Size :

    2 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    On some aerodynamic aspects of the panel flutter problem

    Beranek, R. / Platzer, M. F. / Saunders, L. | NTRS | 1965


    Some effects of system nonlinearities in problem of aircraft flutter

    Woolston, D.S. / Runyan, H.L. / Byrdsong, T.A. | Engineering Index Backfile | 1955


    Mechanism of flutter -- Theoretical and experimental investigation of flutter problem

    Theodorsen, T. / Garrick, I.E. | Engineering Index Backfile | 1940


    General approach to flutter problem

    Loring, S.J. | Engineering Index Backfile | 1941


    Some effects of system nonlinearities in the problem of aircraft flutter

    Woolston, Donald S. / Runyan, Harry L. / Byrdsong, Thomas A. | TIBKAT | 1955