Theoretical and experimental studies on blade-fuselage clearance for higher performance, higher speed helicopters, giving examination for tip-speed ratios approximately equal to 0.3.


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    Title :

    Helicopter blade flapping


    Additional title:

    Aeronautical Eng Rev


    Contributors:

    Published in:

    Publication date :

    1955


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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