Recent applications of the Volterra theory to aeroelastic phenomena

Walter A. Silva, Muhammad R. Hajj, Richard J. Prazenica

Research output: Chapter in Book/Report/Conference proceedingConference contributionpeer-review

Abstract

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.

Original languageEnglish
Title of host publicationIMAC-XXIII
Subtitle of host publicationConference and Exposition on Structural Dynamics - Structural Health Monitoring
StatePublished - 2005
Event23rd Conference and Exposition on Structural Dynamics 2005, IMAC-XXIII - Orlando, FL, United States
Duration: 31 Jan 20053 Feb 2005

Publication series

NameConference Proceedings of the Society for Experimental Mechanics Series
ISSN (Print)2191-5644
ISSN (Electronic)2191-5652

Conference

Conference23rd Conference and Exposition on Structural Dynamics 2005, IMAC-XXIII
Country/TerritoryUnited States
CityOrlando, FL
Period31/01/053/02/05

Fingerprint

Dive into the research topics of 'Recent applications of the Volterra theory to aeroelastic phenomena'. Together they form a unique fingerprint.

Cite this