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contributor authorG. S. Aglietti
contributor authorE. Rogers
date accessioned2017-05-08T21:16:07Z
date available2017-05-08T21:16:07Z
date copyrightJanuary 2003
date issued2003
identifier other%28asce%290893-1321%282003%2916%3A1%2831%29.pdf
identifier urihttp://yetl.yabesh.ir/yetl/handle/yetl/44975
description abstractThis paper describes the validation of a Lagrange-Rayleigh-Ritz technique for the mathematical modeling of mass loaded panels for active control studies. The validation has been carried out by comparing the results produced by a Lagrange-Rayleigh-Ritz model with the results produced by a finite-element model and experimental data. Attention was focussed on a simply supported panel with a lumped mass constrained to its surface to simulate the presence of equipment mounted on the panel and twin piezoelectric patches bonded to the panel, working as sensors and actuators. The design of the experimental rig is described in detail, and a test campaign was carried out to obtain a set of transfer functions characteristic of this plant. The experimental data are then used to validate the predictions of the mathematical model. In particular, it was demonstrated that the Lagrange-Rayleigh-Ritz model was able to reproduce accurately the dynamics of the plant requiring a relatively small number of degrees of freedom.
publisherAmerican Society of Civil Engineers
titleExperimental Validation of Lagrange-Rayleigh-Ritz Modeling Technique for Mass Loaded Actively Controlled Panels
typeJournal Paper
journal volume16
journal issue1
journal titleJournal of Aerospace Engineering
identifier doi10.1061/(ASCE)0893-1321(2003)16:1(31)
treeJournal of Aerospace Engineering:;2003:;Volume ( 016 ):;issue: 001
contenttypeFulltext


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