The identification of nonlinear aeroelastic systems based on the Volterra theory of nonlinear systems is presented. Recent applications of the theory to problems in experimental aeroelasticity are reviewed. These results include the identification of aerodynamic impulse responses, the application of higher-order spectra (HOS) to wind-tunnel flutter data, and the identification of nonlinear aeroelastic phenomena from flight flutter test data of the Active Aeroelastic Wing (AAW) aircraft.


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    Title :

    Recent Applications of the Volterra Theory to Aeroelastic Phenomena


    Contributors:
    W. A. Silva (author) / M. R. Haji (author) / R. J. Prazenica (author)

    Publication date :

    2005


    Size :

    14 pages


    Type of media :

    Report


    Type of material :

    No indication


    Language :

    English







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