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.
Recent Applications of the Volterra Theory to Aeroelastic Phenomena
2005
14 pages
Report
Keine Angabe
Englisch
Aeroelastic System Development Using Proper Orthogonal Decomposition and Volterra Theory
British Library Conference Proceedings | 2003
|Aeroelastic System Development Using Proper Orthogonal Decomposition and Volterra Theory
Online Contents | 2005
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