BUCKLING ANALYSIS OF GENERAL TRIANGULAR ANISOTROPIC PLATES USING POLYNOMIALS

Citation
N. Jaunky et Nf. Knight, BUCKLING ANALYSIS OF GENERAL TRIANGULAR ANISOTROPIC PLATES USING POLYNOMIALS, AIAA journal, 33(12), 1995, pp. 2414-2417
Citations number
19
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
ISSN journal
00011452
Volume
33
Issue
12
Year of publication
1995
Pages
2414 - 2417
Database
ISI
SICI code
0001-1452(1995)33:12<2414:BAOGTA>2.0.ZU;2-Z
Abstract
The problem of buckling of general triangular anisotropic plates with different boundary conditions subjected to combined in-plane loads is considered. Solutions for plate buckling are obtained by using a Rayle igh-Ritz method combined with a variational formulation. The Ritz func tions consist of polynomials that include circulation functions that a re used to impose various boundary conditions. Both classical laminate d-plate theory and first-order shear-deformation theory are used. Nume rical buckling results obtained for isotropic and anisotropic triangul ar plates are compared with results from existing series solutions.