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