An analytical solution to moderately-deep and -thick cylindrical panel
s of rectangular planform, subjected to uniformly distributed transver
se loads, is presented. The shell formulations which include transvers
ely isotropic material (ATJ graphite) properties and Sanders' kinemati
c relations provide five sets of partial differential equations in ter
ms of five unknown displacements. These equations with prescribed geom
etric and natural boundary conditions are solved, following a double F
ourier series approach. Convergence criteria for transverse displaceme
nt and stress couple resultants, and also various parametric effects o
n them, are investigated. Finally, numerical results are compared with
a popular finite element based solution. These numerical results for
such panels and materials should serve as bench-marks for finite eleme
nt and finite difference users.