Experimental validation of a Lagrange-Rayleigh-Ritz modelling technique for mass loaded actively controlled panels


Aglietti, G.S. and Rogers, E. (2003) Experimental validation of a Lagrange-Rayleigh-Ritz modelling technique for mass loaded actively controlled panels Journal of Aerospace Engineering, 16, (1), pp. 31-37. (doi:10.1061/(ASCE)0893-1321(2003)16:1(31)).

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Description/Abstract

This 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.

Item Type: Article
Digital Object Identifier (DOI): doi:10.1061/(ASCE)0893-1321(2003)16:1(31)
ISSNs: 0893-1321 (print)
Keywords: panels, mathematical models, loads
Subjects:
ePrint ID: 22207
Date :
Date Event
2003Published
Date Deposited: 20 Mar 2006
Last Modified: 16 Apr 2017 22:52
Further Information:Google Scholar
URI: http://eprints.soton.ac.uk/id/eprint/22207

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