Dynamic instability of shear-deformable laminated plates

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26 Scopus citations

Abstract

The dynamic instability of antisymmetric angle-ply and cross-ply laminated plates, subjected to periodic inplane loads P(t) = Ps + Pd cosωt, is investigated within the high-order shear deformation lamination theory, where the motion is governed by five partial differential equations. Using the method of multiple-scale, analytical expressions for the instability regions are obtained at ω = Ωj ± Ωi, where Ωi are the natural frequencies of the system. It is shown that, besides the principal instability region at ω = 2Ω11 is the fundamental frequency), other cases of ω = Ωi + Ωj related to the first mode, can be of major importance and yield a significantly enlarged instability region.

Original languageEnglish
Pages (from-to)2000-2005
Number of pages6
JournalAIAA Journal
Volume29
Issue number11
DOIs
StatePublished - 1 Jan 1991

ASJC Scopus subject areas

  • Aerospace Engineering

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