Analysis of smart cross ply laminated shells with shear piezoelectric actuators

Analytical models and solutions are formulated and developed for the static responses of cross ply smart laminated shells with shear piezoelectric actuators. The models are based on a rigorous first-order shell theory. The state-space approach is used to find exact solutions for the static responses...

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Published inSmart materials and structures Vol. 20; no. 10; pp. 105030 - 1-11
Main Authors Khdeir, A A, Aldraihem, O J
Format Journal Article
LanguageEnglish
Published Bristol IOP Publishing 01.10.2011
Institute of Physics
Subjects
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ISSN0964-1726
1361-665X
DOI10.1088/0964-1726/20/10/105030

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Abstract Analytical models and solutions are formulated and developed for the static responses of cross ply smart laminated shells with shear piezoelectric actuators. The models are based on a rigorous first-order shell theory. The state-space approach is used to find exact solutions for the static responses of cross ply spherical, cylindrical and doubly curved shells with various boundary conditions. The smart shells possess two parallel edges simply supported and the remaining ones having any possible combination of boundary conditions: free, clamped or simply supported. Deflections of cross ply laminated shells incorporating shear piezoelectric layers are determined. Numerical results for six layer laminates are generated to investigate the shells' static behavior. The exact solutions for deflections can be used as benchmarks for approximate solutions such as Rayleigh-Ritz and finite element methods.
AbstractList Analytical models and solutions are formulated and developed for the static responses of cross ply smart laminated shells with shear piezoelectric actuators. The models are based on a rigorous first-order shell theory. The state-space approach is used to find exact solutions for the static responses of cross ply spherical, cylindrical and doubly curved shells with various boundary conditions. The smart shells possess two parallel edges simply supported and the remaining ones having any possible combination of boundary conditions: free, clamped or simply supported. Deflections of cross ply laminated shells incorporating shear piezoelectric layers are determined. Numerical results for six layer laminates are generated to investigate the shells' static behavior. The exact solutions for deflections can be used as benchmarks for approximate solutions such as Rayleigh-Ritz and finite element methods.
Author Khdeir, A A
Aldraihem, O J
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Issue 10
Keywords Double curvature
Free boundary
Stratified material
Piezoelectric sensor
Simple support
State space method
Revolution shell
Modeling
Composite material
Static load
Exact solution
Finite element method
Rayleigh Ritz method
Piezoelectric actuators
Piezoelectricity
Ritz method
Cylindrical shell
Shear layer
Structural analysis
Electromechanical properties
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Snippet Analytical models and solutions are formulated and developed for the static responses of cross ply smart laminated shells with shear piezoelectric actuators....
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SubjectTerms Applied sciences
Boundary conditions
Composites
Deflection
Exact sciences and technology
Exact solutions
Forms of application and semi-finished materials
Fundamental areas of phenomenology (including applications)
Laminates
Mathematical analysis
Mathematical models
Physics
Polymer industry, paints, wood
Shear
Shells
Solid mechanics
Structural and continuum mechanics
Technology of polymers
Title Analysis of smart cross ply laminated shells with shear piezoelectric actuators
URI http://iopscience.iop.org/0964-1726/20/10/105030
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Volume 20
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