BUCKLING OF RECTANGULAR SYMMETRICAL ANGLE-PLY LAMINATED PLATES DETERMINED BY EIGENSENSITIVITY ANALYSIS

Authors
BARTON O REISS R
Citation
O. Barton et R. Reiss, BUCKLING OF RECTANGULAR SYMMETRICAL ANGLE-PLY LAMINATED PLATES DETERMINED BY EIGENSENSITIVITY ANALYSIS, AIAA journal, 33(12), 1995, pp. 2406-2413
Citations number
16
Categorie Soggetti
Aerospace Engineering & Tecnology
Journal title
AIAA journal → ACNP
ISSN journal
00011452
Volume
33
Issue
12
Year of publication
1995
Pages
2406 - 2413
Database
ISI
SICI code
0001-1452(1995)33:12<2406:BORSAL>2.0.ZU;2-F
Abstract
Closed-form approximate solutions for uniaxial and biaxial compressive buckling of rectangular symmetric angle-ply laminates are developed f rom eigensensitivity analysis. Boundary conditions, which consist of t he various combinations of clamped and simply supported edges, are inc orporated through appropriate edge condition parameters. Calculated re sults, presented for elastic moduli ratios up to 40, compare quite fav orably with the corresponding buckling loads obtained from the Ritz me thod.