In Part 1 it is shown that the equation for blade equilibrium about the flapping pin is


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    Title :

    Rotor Blade Motion in a Vertical Sharp-edged Gust


    Subtitle :

    A Study of the Dynamics of Helicopter Blade Flapping with a Method of Deriving Maximum Gust Deflexion


    Contributors:
    Payne, P.R. (author)


    Publication date :

    1954-02-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Rotor Blade Motion in a Vertical Sharp-Edged Gust

    Payne, P.R. | Emerald Group Publishing | 1954


    Rotor Blade Motion in a Vertical Sharp-edged Gust

    Payne, P.R. | Emerald Group Publishing | 1954



    Effects of wing twist on response of airplane encountering sharp-edged gust

    Yeh, G.C.K. / Martinek, J. | Engineering Index Backfile | 1953