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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    Title :

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


    Contributors:

    Publication date :

    1969


    Size :

    66 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English





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