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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    Title :

    Application of absorber to reduce helicopter vibration levels


    Additional title:

    Am Helicopter Soc -- J


    Contributors:
    Ellis, C.W. (author) / Jones, R. (author)


    Publication date :

    1963


    Size :

    9 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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