Novel form of flutter is explained and investigated; existence of instability is demonstrated with mathematical model of aircraft; problem is investigated by use of Lagrange's Equations of Motion and Nyquist stability criterion for servo mechanisms; method is applied to elevator system controlling pitch-plane motion of simplified aircraft having gyroscope feedback.


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    Title :

    Flutter of aircraft controlled by automatic navigation system


    Additional title:

    Roy Aeronautical Soc -- J


    Contributors:
    Parks, P.C. (author)

    Published in:

    Publication date :

    1961


    Size :

    6 pages


    Type of media :

    Article (Journal)


    Type of material :

    Print


    Language :

    English


    Keywords :



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