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