Rotor enables much higher speeds with conventional helicopter; penalty paid for this in form of hub pitching moments which have to be balanced out externally either by use of two rotors, offset CG, aerodynamic surfaces, or inclination of mechanical axis; equations developed for calculating blade elemental angle of attack, claimed to be superior to classic methods for design office purposes. (See also - v 26 n 309 Nov 1954 p 378-82)


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    Titel :

    High offset flapping pin rotor analysis


    Weitere Titelangaben:

    Aircraft Eng


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

    Erschienen in:

    Erscheinungsdatum :

    1955


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


    High Offset Flapping Pin Rotor Analysis

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