Development of vibration absorber for reduction of helicopter vibration levels by Kaman Aircraft Corp, Bloomfield, Conn, and approach taken; test results show that absorber installation can effectively eliminate structural amplification of predominant flight vibration frequencies without transferring vibration problem to other areas in aircraft; design problems connected with absorber installation are easily resolved, and service results satisfactory.


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    Titel :

    Application of absorber to reduce helicopter vibration levels


    Weitere Titelangaben:

    Am Helicopter Soc -- J


    Beteiligte:
    Ellis, C.W. (Autor:in) / Jones, R. (Autor:in)


    Erscheinungsdatum :

    1963


    Format / Umfang :

    9 pages


    Medientyp :

    Aufsatz (Zeitschrift)


    Format :

    Print


    Sprache :

    Englisch


    Schlagwörter :


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