THERMAL BUCKLING OF CROSS-PLY COMPOSITE LAMINATES USING A 1ST-ORDER SHEAR DEFORMATION-THEORY

Authors
ABRAMOVICH H
Citation
H. Abramovich, THERMAL BUCKLING OF CROSS-PLY COMPOSITE LAMINATES USING A 1ST-ORDER SHEAR DEFORMATION-THEORY, Composite structures, 28(2), 1994, pp. 201-213
Citations number
12
Categorie Soggetti
Materials Sciences, Composites
Journal title
Composite structures → ACNP
ISSN journal
02638223
Volume
28
Issue
2
Year of publication
1994
Pages
201 - 213
Database
ISI
SICI code
0263-8223(1994)28:2<201:TBOCCL>2.0.ZU;2-3
Abstract
Thermal buckling of symmetric and non-symmetric cross-ply composite la minated beams is investigated based on a first-order shear deformation theory. Detailed analytical analysis is carried out for the thermal b uckling parameter of laminated beams made out of Kevlar-epoxy, carbon- epoxy and glass-epoxy. The results are presented for various boundary conditions, lay-up sequences, slenderness ratios and transverse shear moduli.