Helicopter tail rotors are subject to many types of divergent vibration. A classification of these various types is presented, and a description given of those which have been actually observed. The means used by manufacturers to predict and avoid such vibrations include various calculations in the design stage and special test stands for development work. Substantiation tests accomplished on these stands enable flight tests to be undertaken with a tail rotor free from divergent vibrations.


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    Titel :

    Divergent Vibration in Helicopter Tail Rotors


    Weitere Titelangaben:

    Sae Technical Papers


    Beteiligte:
    Normand, Y. (Autor:in)

    Kongress:

    1965 International Automotive Engineering Congress and Exposition ; 1965



    Erscheinungsdatum :

    01.02.1965




    Medientyp :

    Aufsatz (Konferenz)


    Format :

    Print


    Sprache :

    Englisch





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