NASA Logo

NTRS

NTRS - NASA Technical Reports Server

Press Enter or click the Search button to begin your search.

Back to Results
Modeling of Structural-Acoustic Interaction Using Coupled FE/BE Method and Control of Interior Acoustic Pressure Using Piezoelectric ActuatorsA coupled finite element (FE) and boundary element (BE) approach is presented to model full coupled structural/acoustic/piezoelectric systems. The dual reciprocity boundary element method is used so that the natural frequencies and mode shapes of the coupled system can be obtained, and to extend this approach to time dependent problems. The boundary element method is applied to interior acoustic domains, and the results are very accurate when compared with limited exact solutions. Structural-acoustic problems are then analyzed with the coupled finite element/boundary element method, where the finite element method models the structural domain and the boundary element method models the acoustic domain. Results for a system consisting of an isotropic panel and a cubic cavity are in good agreement with exact solutions and experiment data. The response of a composite panel backed cavity is then obtained. The results show that the mass and stiffness of piezoelectric layers have to be considered. The coupled finite element and boundary element equations are transformed into modal coordinates, which is more convenient for transient excitation. Several transient problems are solved based on this formulation. Two control designs, a linear quadratic regulator (LQR) and a feedforward controller, are applied to reduce the acoustic pressure inside the cavity based on the equations in modal coordinates. The results indicate that both controllers can reduce the interior acoustic pressure and the plate deflection.
Document ID
19970024872
Acquisition Source
Langley Research Center
Document Type
Contractor Report (CR)
Authors
Mei, Chuh
(Old Dominion Univ. Norfolk, VA United States)
Shi, Yacheng
(Old Dominion Univ. Norfolk, VA United States)
Date Acquired
September 6, 2013
Publication Date
August 1, 1997
Subject Category
Acoustics
Report/Patent Number
NASA-CR-204986
NAS 1.26:204986
ODURF-151651
Report Number: NASA-CR-204986
Report Number: NAS 1.26:204986
Report Number: ODURF-151651
Accession Number
97N24585
Funding Number(s)
CONTRACT_GRANT: NAG1-1684
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
No Preview Available