SUMMARY A detailed account is given of the aerodynamic and inertia forces acting on a rotor blade when the helicopter is undergoing arbitrary disturbance in velocity and angular velocity. A fairly generalized form is used for the downwash velocity. A principle is enunciated enabling the several second order terms of significance in the angle variables to be recognized and retained.


    Access

    Check access

    Check availability in my library

    Order at Subito €


    Export, share and cite



    Title :

    Rotor Dynamics and Helicopter Stability


    Subtitle :

    Development of a Unified Mathematical Theory of the Steady and Disturbed Motion of a Helicopter with Particular Emphasis on the Dynamical Aspects of the Problem


    Contributors:
    Price, H.L. (author)

    Published in:

    Publication date :

    1963-06-01


    Size :

    5 pages




    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    English



    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1963


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1964


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1964


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1963


    Rotor Dynamics and Helicopter Stability

    Price, H.L. | Emerald Group Publishing | 1965