Main barrier to higher rotary wing cruising speeds is condition of flow over retreating side of disk; logical solution is to unload only that portion of disk where flow conditions are detrimental to higher speeds, and stiff hinged rotor is suggested as means of doing this. (See also Aircraft Eng v 27 n 321 Nov 1955 p 358-70)


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    Titel :

    Stiff-hinged helicopter rotor


    Weitere Titelangaben:

    Flight


    Beteiligte:
    Payne, P.R. (Autor:in)

    Erschienen in:

    Flight ; 68 , n 2438


    Erscheinungsdatum :

    1955


    Format / Umfang :

    3 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    Stiff-hinged helicopter rotor

    Payne, P.R. | Engineering Index Backfile | 1955


    The Stiff-hinged Helicopter Rotor

    Payne, P.R. | Emerald Group Publishing | 1955




    Stability and Control of Single Rotor Helicopter with Hinged Blades

    Zbrozek, J.K. | Emerald Group Publishing | 1949