The results of study and evaluation of a new design concept for helicopter tail rotors are reported. The evaluation was conducted by means of a whirl test which included separate runs at full pitch (19 DEG), overspeed to 110% rpm, and simulated forward flight to 105 knots. (Author)


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    Titel :

    Study and Evaluation of Directed Glass Fiber Reinforced Plastic Helicopter Tail Rotor Assembly


    Beteiligte:
    P. F. Maloney (Autor:in) / F. B. Clark (Autor:in) / H. H. McIntyre (Autor:in)

    Erscheinungsdatum :

    1969


    Format / Umfang :

    66 pages


    Medientyp :

    Report


    Format :

    Keine Angabe


    Sprache :

    Englisch





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