Although stability failure of constant thickness plates is a fairly well un
derstood problem, buckling of plates with varying thickness has seen little
research. This is not a common problem, but buckling of varying thickness
plates does occur, as in the case of Advanced Grid Stiffened structures. Th
ese structures are characterized by lattices of rigidly connected rib stiff
eners. While real-world Advanced Grid Stiffened structure ribs are modeled
as orthotropic plates, they often have complex cross-sections (i.e., varyin
g thickness). Unfortunately, failure analysis techniques for these ribs hav
e been limited to rectangular cross-sections. To address this shortcoming,
a buckling theory is presented for orthotropic plates of varying thickness.
Orthotropic plates with both linear and hourglass thickness variations are
considered. These are common grid structure cross-section geometries resul
ting from existing manufacturing processes. For both geometries, results ar
e given that allow designers to predict how these plates will behave, relat
ive to a constant thickness plate, for a variety of material properties and
plate aspect ratios.