Active flutter control of thin walled wing-engine system using piezoelectric actuators

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dc.authoridasadi, davood/0000-0002-2066-6016
dc.authoridFarsadi, Turac/0009-0002-8382-0313
dc.contributor.authorAsadi, Davood
dc.contributor.authorFarsadi, Touraj
dc.date.accessioned2025-01-06T17:36:05Z
dc.date.available2025-01-06T17:36:05Z
dc.date.issued2020
dc.description.abstractIn the present study, control of a Thin Walled Beam (TWB) wing-engine system is examined applying piezoelectric actuators to enhance the performance of aeroelastic response. The composite piezoelectric governing equations of motion including the structure and electric effects are derived applying Hamilton's principle. Piezoelectric composite plate equations are added to the composite host wing-engine governing system of equations. The incompressible aerodynamic model based on Wagner's function is applied and the Ritz based solution methodology is employed. As a passive control approach, the effects of piezoelectric fiber angles are studied on the time domain response of the high-aspect-ratio wing-engine system. The linear quadratic Gaussian (LQG) control algorithm is applied as a closed-loop active control strategy to enhance the flutter response characteristics of the composite wing-engine system. Numerical results firstly, demonstrate the effectiveness of the active control strategy based on piezocomposite actuator on suppressing the flutter response of the composite wing-engine system and secondly, prove the effect of piezocomposite actuator location and fiber angle orientation on the closed-loop control performance. (C) 2020 Elsevier Masson SAS. All rights reserved.
dc.identifier.doi10.1016/j.ast.2020.105853
dc.identifier.issn1270-9638
dc.identifier.issn1626-3219
dc.identifier.scopus2-s2.0-85084940268
dc.identifier.scopusqualityQ1
dc.identifier.urihttps://doi.org/10.1016/j.ast.2020.105853
dc.identifier.urihttps://hdl.handle.net/20.500.14669/1741
dc.identifier.volume102
dc.identifier.wosWOS:000538117700001
dc.identifier.wosqualityQ1
dc.indekslendigikaynakWeb of Science
dc.indekslendigikaynakScopus
dc.language.isoen
dc.publisherElsevier France-Editions Scientifiques Medicales Elsevier
dc.relation.ispartofAerospace Science and Technology
dc.relation.publicationcategoryMakale - Uluslararası Hakemli Dergi - Kurum Öğretim Elemanı
dc.rightsinfo:eu-repo/semantics/closedAccess
dc.snmzKA_20241211
dc.subjectActive control
dc.subjectPiezoelectric
dc.subjectFlutter
dc.subjectComposite wing-engine system
dc.titleActive flutter control of thin walled wing-engine system using piezoelectric actuators
dc.typeArticle

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