Results of investigation made by Cornell Aeronautical Laboratory are presented; rotor configuration studied utilizes jet-flap for cyclic and collective pitch control as well as for propulsion; effects of blade center-of-gravity position, bending-to-torsional frequency ratio, advance ratio and control-flap characteristics on aeroelastic characteristics of rotor system are reviewed.


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    Titel :

    Aeroelastic characteristics for jet-flap helicopter rotor in forward flight


    Weitere Titelangaben:

    SAE -- Paper


    Beteiligte:
    White, Jr., R.P. (Autor:in) / Trenka, A.R. (Autor:in)

    Kongress:

    SAE Meeting ; 1962



    Erscheinungsdatum :

    1962


    Format / Umfang :

    36 pages


    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :