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Coupled mixed-field laminate theory and finite element for smart piezoelectric composite shell structuresMechanics for the analysis of laminated composite shells with piezoelectric actuators and sensors are presented. A new mixed-field laminate theory for piezoelectric shells is formulated in curvilinear coordinates which combines single-layer assumptions for the displacements and a layerwise representation for the electric potential. The resultant coupled governing equations for curvilinear piezoelectric laminates are described. Structural mechanics are subsequently developed and an 8-node finite-element is formulated for the static and dynamic analysis of adaptive composite structures of general laminations containing piezoelectric layers. Evaluations of the method and comparisons with reported results are presented for laminated piezoelectric-composite plates, a closed cylindrical shell with a continuous piezoceramic layer and a laminated composite semi-circular cantilever shell with discrete cylindrical piezoelectric actuators and/or sensors.
Document ID
19960041440
Acquisition Source
Legacy CDMS
Document Type
Contractor Report (CR)
Authors
Saravanos, Dimitris A.
(Ohio Aerospace Inst. Brook Park, OH United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1996
Subject Category
Structural Mechanics
Report/Patent Number
NAS 1.26:198490
E-10276
NASA-CR-198490
Accession Number
96N31384
Funding Number(s)
PROJECT: RTOP 505-63-5B
CONTRACT_GRANT: NCC3-391
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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