Method for solution of class of Hill differential equations is applied to solution of equation for flapping motion of helicopter rotor blades; stability of blade flapping motion is established for range of numerical parameters usually arising in helicopter theory.


    Access

    Access via TIB

    Check availability in my library


    Export, share and cite



    Title :

    Rotor blade flapping motion


    Additional title:

    Brown Univ -- Quarterly Applied Mathematics


    Contributors:
    Horvay, G. (author)

    Published in:

    Publication date :

    1947


    Size :

    19 pages


    Remarks:

    Bibliography


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


    The stability of rotor blade flapping motion

    Shutler, A. G. / Jones, J. P. | TIBKAT | 1961


    The stability of rotor blade flapping motion

    Shutler, A. G. ;Jones, J. P. | SLUB | 1961


    Measurement of rotor blade flapping

    DILLON JOHN A | European Patent Office | 2018

    Free access


    Helicopter Rotor Blade Flapping and Bending

    Jones, J.P. | Emerald Group Publishing | 1957