Stall flutter of helicopter rotor in simulated forward flight was found to occur in all forward flight cases involving appreciable blade stall, and consisted almost entirely of blade motion in torsional mode; stall flutter amplitude was found to be dependent on such parameters as blade chordwise center of gravity position, torsional damping, torsional frequency, and degree of stall occuring over rotor disk.


    Zugriff

    Zugriff über TIB

    Verfügbarkeit in meiner Bibliothek prüfen


    Exportieren, teilen und zitieren



    Titel :

    Experimental investigation of stall flutter


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Ham, N.D. (Autor:in)


    Erscheinungsdatum :

    1962


    Format / Umfang :

    14 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Stall Flutter

    F. Sisto | NTIS | 1987


    Stall-Flutter Analysis

    Lars E. Ericsson / J. Peter Reding | AIAA | 1973


    Stall flutter analysis

    ERICSSON, L. / REDING, J. | AIAA | 1972


    Unsteady airfoil stall and stall flutter

    Ericsson, L. E. / Reding, J. P. | NTRS | 1971


    Stall flutter analysis.

    Ericsson, L. E. / Reding, J. P. | NTRS | 1972