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 = 2Ω1 (Ω1 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 language | English |
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Pages (from-to) | 2000-2005 |
Number of pages | 6 |
Journal | AIAA Journal |
Volume | 29 |
Issue number | 11 |
DOIs | |
State | Published - 1 Jan 1991 |
ASJC Scopus subject areas
- Aerospace Engineering