FREE-VIBRATION ANALYSIS OF LAMINATED PLATES USING A LAYERWISE THEORY

Citation
A. Nosier et al., FREE-VIBRATION ANALYSIS OF LAMINATED PLATES USING A LAYERWISE THEORY, AIAA journal, 31(12), 1993, pp. 2335-2346
Citations number
18
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00011452
Volume
31
Issue
12
Year of publication
1993
Pages
2335 - 2346
Database
ISI
SICI code
0001-1452(1993)31:12<2335:FAOLPU>2.0.ZU;2-#
Abstract
Reddy's layerwise theory is used to perform free-vibration analysis of laminated plates. This theory is the most current and sophisticated t heory in which full account is given to various three-dimensional effe cts. The results obtained from this theory are compared with those obt ained from a full-fledged three-dimensional elasticity analysis and va rious equivalent single-layer theories that are available. These inclu de the classical laminated plate theory (CLPT), the first-order shear deformation laminated plate theory (FSDPT), and the third-order shear deformation plate theory (THSDPT). The elasticity equations are solved by utilizing the state-space variables and the transfer matrix. A det ailed analysis is carried out, by uncoupling the Navier equations, to study the various mode shapes and natural frequencies of a homogeneous transversely isotropic plate. Results are also obtained for symmetric and antisymmetric cross-ply laminates.