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.


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    Titel :

    Rotor Dynamics and Helicopter Stability


    Untertitel :

    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


    Beteiligte:
    Price, H.L. (Autor:in)

    Erschienen in:

    Erscheinungsdatum :

    1963-06-01


    Format / Umfang :

    5 pages




    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Elektronische Ressource


    Sprache :

    Englisch



    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 | 1963


    Rotor Dynamics and Helicopter Stability

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