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Analysis of laminated composite plates using a higher-order shear deformation theory

โœ Scribed by N. D. Phan; J. N. Reddy


Publisher
John Wiley and Sons
Year
1985
Tongue
English
Weight
852 KB
Volume
21
Category
Article
ISSN
0029-5981

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โœฆ Synopsis


A higher-order shear deformation theory is used to analyse laminated anisotropic composite plates for deflections, stresses, natural frequencies and buckling loads. The theory accounts for parabolic distribution of the transverse shear stresses, and requires no shear correction coefficients. A displacement finite element model of the theory is developed, and applications of the clement to bending, vibration and stability of laminated plates are discussed. The present solutions are compared with those obtained using the classical plate theory and the three-dimensional elasticity theory.


๐Ÿ“œ SIMILAR VOLUMES


Vibration Analysis Of Laminated Plates U
โœ J.-F. He; B.-A. Ma ๐Ÿ“‚ Article ๐Ÿ“… 1994 ๐Ÿ› Elsevier Science ๐ŸŒ English โš– 373 KB

A previously published discrete-layer shear deformation theory is used to analyze free vibration of laminated plates. The theory includes the assumption that the transverse shear strains across any two layers are linearly dependent on each other. The theory has the same dependent variables as first