THE nature of the instability of helicopters is described here by Mr. Kelley, who also enumerates factors that contribute to it.Two of Arthur M. Young's early attempts to solve the problem are discussed by the author, who states that the final solution is a device that makes model helicopters perfectly stable in flight.The application of this device to full-scale helicopters is also described.


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    Titel :

    HELICOPTER STABILITY with Young's Lifting Rotor


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:

    Kongress:

    Pre-1964 SAE Technical Papers ; 1906



    Erscheinungsdatum :

    1945-01-01




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Helicopter stability with Young's lifting rotor

    Kelley, B. | Engineering Index Backfile | 1945


    Non-linear helicopter rotor lifting surface theory

    Csencsitz, T. | Tema Archiv | 1974


    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