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.