Structures consisting of thin plates stiffened by a system of ribs or diaph
ragms form a class of structural elements of practical importance in variou
s engineering applications. A differential quadrature analysis of free vibr
ation of plates with eccentric stiffeners is presented. The plate and the s
tiffeners are treated separately. Simultaneous governing differential equat
ions are derived from the plate dynamic equilibrium, the stiffener dynamic
equilibrium, and equilibrium and compatibility conditions along the interfa
ce of a plate segment and a stiffener. The plate and the stiffeners have di
splacements in three dimensions. Shear forces and in-plane forces in the pl
ate are considered to satisfy the compatibility at the interface of a plate
segment and a stiffener. Meanwhile, in-plane inertia effects in the plate
and in the stiffener are ignored. The application of the differential quadr
ature method is demonstrated by three examples: a simply supported plate wi
th central eccentric stiffener, a clamped square plate with central eccentr
ic stiffener., and a double-ribbed plate with all edges clamped. The natura
l frequencies are compared with the experimental results. and with the resu
lts obtained by finite element analysis. Very good agreement was found. (C)
2001 Academic Press.