Analysis of composite plates using various plate theories -Part 1: Formulation and analytical solutions

Bose, P.S.C.; Jn, Reddy

doi:10.12989/sem.1998.6.6.583

Cited by 72 publications

(34 citation statements)

References 98 publications

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“…Later using the above three models, Ramalingeswara and Ganesan [53] compared the results of interlaminar stresses in a crossply spherical shell subjected to uniform transverse pressure. Recently a comparison of the analytical solutions of a few laminated plate theories for the analysis of multilayer composite plates were presented by Idlbi et al [54] Carvelli and Savoia, [55] Bose and Reddy [56].…”

Section: Methodsmentioning

confidence: 99%

Estimation of transverse/interlaminar stresses in laminated composites – a selective review and survey of current developments

Kant

Swaminathan

2000

Composite Structures

269

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A review is made on the dierent methods used for the estimation of transverse/interlaminar stresses in laminated composite plates and shells. Both analytical and numerical methods are considered. In numerical methods while the emphasis is given on ®nite element methods, other methods like the ®nite dierence method is also brie¯y discussed. Aspects considered are: eects of variation in geometric and material parameters, transverse shear and normal deformation, interface stress continuity and the interfacial bonding on the accuracy of prediction of transverse/interlaminar stresses. Finally some general conclusions are presented along with future directions of research on the analysis of multilayered composite plates and shells for free-edge eects.

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Section: Methodsmentioning

confidence: 99%

Estimation of transverse/interlaminar stresses in laminated composites – a selective review and survey of current developments

Kant

Swaminathan

2000

Composite Structures

269

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“…The classical laminate plate theory (CLPT) [1] is only suitable for thin plates. The first-order shear deformation theory (FSDT) [2], which shear deformation effect is regarded, can be applied for both moderately thick and thin plates.…”

Section: Accepted Manuscriptmentioning

confidence: 99%

Isogeometric analysis of laminated composite and sandwich plates using a new inverse trigonometric shear deformation theory

Thai

Ferreira

Bordas

et al. 2014

European Journal of Mechanics - A/Solids

280

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“…The in-plane displacements u and v are now expressed as complete cubic powers in the thickness coordinate z. A complete account on the various forms of higher-order shear deformation plate theories is given by Bose and Reddy [26].…”

Section: Higher-order Displacement Fieldsmentioning

confidence: 99%

Buckling analysis of composite laminates under end shortening by higher‐order shear deformable finite strips

Zou

Lam

2002

Numerical Meth Engineering

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SUMMARYA higher-order shear deformable ÿnite strip is developed and employed in the buckling analysis of laminated composite plates when subjected to uniform end shortening. This enables the transverse shear deformation to be accurately incorporated. The permitted laminate material properties are quite general, encompassing anisotropy and full coupling between in-plane and out-of-plane behaviour. Results with respect to the number of plies, thickness of laminate and ratios of E 11 =E 22 are presented for unsymmetric cross-ply and angle-ply lay-ups and for laminates with arbitrary lay-up arrangements.

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Analysis of composite plates using various plate theories -Part 1: Formulation and analytical solutions

Cited by 72 publications

References 98 publications

Estimation of transverse/interlaminar stresses in laminated composites – a selective review and survey of current developments

Estimation of transverse/interlaminar stresses in laminated composites – a selective review and survey of current developments

Isogeometric analysis of laminated composite and sandwich plates using a new inverse trigonometric shear deformation theory

Buckling analysis of composite laminates under end shortening by higher‐order shear deformable finite strips

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