Vibration and buckling of generally laminated composite plates with arbitrary edge conditions

DOI10.1016/0020-7403(87)90026-9zbMath0622.73064OpenAlexW2034238788MaRDI QIDQ1091179

B. Baharlou, Arthur W. Leissa

Publication date: 1987

Published in: International Journal of Mechanical Sciences (Search for Journal in Brave)

Full work available at URL: https://doi.org/10.1016/0020-7403(87)90026-9

zbMATH Keywords

algorithmbendingpolynomialsRitz methodfree vibrationclampedsimply supportedDisplacement functionsstrain energy functionalarbitrary edge conditionsarbitrary ply stacking sequencesgenerally laminated composite platesgeometric boundary conditionsstretching effects

Mathematics Subject Classification ID

Vibrations in dynamical problems in solid mechanics (74H45) Plates (74K20) Composite and mixture properties (74E30) Bifurcation and buckling (74G60) Nonlinear constitutive equations for materials with memory (74D10)

Related Items (7)

Free vibration of functionally graded sandwich plates using four-variable refined plate theory ⋮ Dynamics of solid propellant motor composite casing under impact pressure ⋮ The buckled states of annular sandwich plates ⋮ Stochastic dynamic stability analysis of composite curved panels subjected to non-uniform partial edge loading ⋮ Thin plate spline radial basis functions for vibration analysis of clamped laminated composite plates ⋮ Analysis of Laminates using Multiquadric Radial Basis Function ⋮ Local buckling of wide-flange thin-walled anisotropic composite beams

This page was built for publication: Vibration and buckling of generally laminated composite plates with arbitrary edge conditions