Existence of flutter in such craft depends, in part, on dynamic characteristics of servomechanism used for control; method evolved wherein impedance of servo and related elastic structure, as obtained by test, is compared to set of theoretical flutter boundary curves.


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    Title :

    Flutter of servo-controlled aircraft


    Additional title:

    J Aeronautical Sciences


    Contributors:
    Winson, J. (author)


    Publication date :

    1949


    Size :

    8 pages


    Remarks:

    Charts


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :


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