Effect of face-sheet anisotropy on buckling and postbuckling of sandwich plates

Citation
T. Hause et al., Effect of face-sheet anisotropy on buckling and postbuckling of sandwich plates, J SPAC ROCK, 37(3), 2000, pp. 331-341
Citations number
16
Categorie Soggetti
Aereospace Engineering
Journal title
JOURNAL OF SPACECRAFT AND ROCKETS
ISSN journal
00224650 → ACNP
Volume
37
Issue
3
Year of publication
2000
Pages
331 - 341
Database
ISI
SICI code
0022-4650(200005/06)37:3<331:EOFAOB>2.0.ZU;2-6
Abstract
A study of the effect of anisotropy of face sheets on buckling and postbuck ling of sandwich flat panels subjected to both mechanical and thermal loads is presented. The mechanical loads consist of uniaxial compressive/tensile edge loads, while the temperature is assumed to exhibit an antisymmetric v ariation through the panel thickness. The study is carried out in the conte xt of a geometrically nonlinear theory of sandwich structures that also inc orporates the effect of unavoidable stress-free initial geometric imperfect ions. A detailed analysis of the influence of a large number of parameters associated with the panel geometry, material properties of the core, fiber orientation and stacking sequence in the face sheet, and character of tange ntial boundary conditions (i.e., movable or immovable) on buckling strength and postbuckling response is accomplished, and pertinent conclusions are o utlined.