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Mechanics of Composite Materials
Erschienen in: Mechanics of Composite Materials 2/2016

06.05.2016

A Simple Finite Element with Five Degrees of Freedom Based on Reddy’s Third-Order Shear Deformation Theory

verfasst von: K. Belkaid, A. Tati, R. Boumaraf

Erschienen in: Mechanics of Composite Materials | Ausgabe 2/2016

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Abstract

A simple four-node isoparametric finite element with five degrees of freedom, based on Reddy’s third-order shear deformation theory, is elaborated and used in a model for analizing the bending of laminated plates. The results obtained are compared with solutions given by the three-dimensional elasticity and other theories.
Vorheriger Artikel Influence of the Interaction Between Fibers Periodically Located in a Composite Material on the Distribution of Stresses in It
Nächster Artikel Load-Carrying Capacity of a Fiber-Reinforced Annular Tree-Layer Composite Plate Clamped on its External and Internal Contours

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Metadaten
Titel
A Simple Finite Element with Five Degrees of Freedom Based on Reddy’s Third-Order Shear Deformation Theory
verfasst von
K. Belkaid
A. Tati
R. Boumaraf
Publikationsdatum
06.05.2016
Verlag
Springer US
Erschienen in
Mechanics of Composite Materials / Ausgabe 2/2016
Print ISSN: 0191-5665
Elektronische ISSN: 1573-8922
DOI
https://doi.org/10.1007/s11029-016-9578-z

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