– an angle of attack of the main rotor). The vortex ring state has been considered also.


    Access

    Download


    Export, share and cite



    Title :

    THE INVESTIGATION OF ROTOR’S INFLOW AND MAIN ROTOR’S INDUCED VELOCITY AT HOVER AND AT STEEP DESCENTS


    Contributors:


    Publication date :

    2016



    Type of media :

    Article (Journal)


    Type of material :

    Electronic Resource


    Language :

    Unknown




    Download - The tilt rotor's downfall

    Chana, William / Sullivan, T. | AIAA | 1993


    SPECIALTY OF ROTOR’S DRIVE MECHANISM OSCILLATIONS

    V. S. Loveikin / Yu. V. Chovnyuk / A. P. Lyashko | DOAJ | 2016

    Free access

    93-4814 Download - The Tilt Rotor's Downfall

    Chana, W. / Sullivan, T. / American Institute of Aeronautics and Astronautics | British Library Conference Proceedings | 1993



    Modelling a helicopter rotor's response to wake encounters

    Whitehouse, G.R. | Online Contents | 2004