The document is comprised of 27 papers grouped under the following headings: The state-of-the-art; Flight dynamics of a flexible VTOL rotor; Flight dynamics of flexible airplanes (theoretical methods); Experimental methods for flight dynamics of the flexible airplane; Stability and control augmentation devices.


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    Title :

    Aeroelastic Effects from a Flight Mechanics Standpoint


    Publication date :

    1970


    Size :

    415 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English