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Coupled electromechanical response of composite beams with embedded piezoelectric sensors and actuatorsUnified mechanics are developed with the capability to model both sensory and active composite laminates with embedded piezoelectric layers. A discrete-layer formulation enables analysis of both global and local electromechanical response. The mechanics include the contributions from elastic, piezoelectric, and dielectric components. The incorporation of electric potential into the state variables permits representation of general electromechanical boundary conditions. Approximate finite element solutions for the static and free-vibration analysis of beams are presented. Applications on composite beams demonstrate the capability to represent either sensory or active structures and to model the complicated stress-strain fields, the interactions between passive/active layers, interfacial phenomena between sensors and composite plies, and critical damage modes in the material. The capability to predict the dynamic characteristics under various electrical boundary conditions is also demonstrated.
Document ID
19940029393
Acquisition Source
Legacy CDMS
Document Type
Conference Paper
Authors
Saravanos, D. A.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Heyliger, P. R.
(Ohio Aerospace Inst. Brook Park, OH, United States)
Date Acquired
September 6, 2013
Publication Date
June 1, 1994
Subject Category
Composite Materials
Report/Patent Number
E-8728
NAS 1.26:195313
NASA-CR-195313
Report Number: E-8728
Report Number: NAS 1.26:195313
Report Number: NASA-CR-195313
Meeting Information
Meeting: ASME Winter Annual Meeting
Location: New Orleans, LA
Country: United States
Start Date: November 28, 1993
End Date: December 3, 1993
Sponsors: ASME
Accession Number
94N33899
Funding Number(s)
CONTRACT_GRANT: NCC3-208
PROJECT: RTOP 505-63-5B
Distribution Limits
Public
Copyright
Work of the US Gov. Public Use Permitted.
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