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Buckling of symmetrically laminated plates with compression, shear, and in-plane bending

Authors :
Michael P. Nemeth
Source :
AIAA Journal. 30:2959-2965
Publication Year :
1992
Publisher :
American Institute of Aeronautics and Astronautics (AIAA), 1992.

Abstract

A parametric study of the buckling behavior of infinitely long symmetrically laminated anisotropic plates subjected to combined loadings is presented. The loading conditions considered are pure in-plane bending, transverse tension and compression, and shear. Results obtained using a special purpose analysis that is well suited for parametric studies are presented for clamped and simply supported plates. Moreover, results are presented for some common laminate constructions, and generic buckling design charts are presented for a wide range of useful nondimensional parameters.

Details

ISSN :
1533385X and 00011452
Volume :
30
Database :
OpenAIRE
Journal :
AIAA Journal
Accession number :
edsair.doi...........675954ff30a7f4cf42a45c0ef65c1c0a
Full Text :
https://doi.org/10.2514/3.11643