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A remark on the state-space concept applied to bending, buckling and free vibration of composite laminates
Date
1996-06-03
Author
Khdeir, AA
Metadata
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Creative Commons Attribution-NonCommercial-NoDerivatives 4.0 International License
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The present study shows that the state-space concept used to generate exact solutions for various boundary conditions for bending, buckling and free vibration of composite laminates, can be modified easily and exactly and has no drawback when the laminate thickness is reduced. Numerical results for central deflections, axial stresses, transverse shear stresses, critical buckling loads and natural frequencies of cross-ply laminated plates are obtained using the classical, first- and third-order theories for large side to thickness ratios. Copyright (C) 1996 Elsevier Science Ltd.
Subject Keywords
Circular Cylindrical-Shells
,
Plate Theories
,
Ply
,
Stability
URI
https://hdl.handle.net/11511/63401
Journal
COMPUTERS & STRUCTURES
DOI
https://doi.org/10.1016/0045-7949(95)00330-4
Collections
Department of Civil Engineering, Article
Citation Formats
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BibTeX
A. Khdeir, “A remark on the state-space concept applied to bending, buckling and free vibration of composite laminates,”
COMPUTERS & STRUCTURES
, vol. 59, no. 5, pp. 813–817, 1996, Accessed: 00, 2020. [Online]. Available: https://hdl.handle.net/11511/63401.