A two degree-of-freedom model, consisting of a rigid rotor supported o
n rigid bearings which are in turn supported on squeeze film dampers,
is considered. Isotropic centering springs are assumed resulting in a
steady synchronous centered circular response for the rotor. The resul
ting nonlinear system is modeled in non-dimensional form. The transmis
sibility ratio of the system as well as the power dissipated are minim
ized for various values of unbalance and at several speeds, with the s
queeze film bearing parameter as the primary design variable. Expressi
ons are derived for linear variational stability of the circular orbit
, and are imposed as constraints in the optimization process. The depe
ndence of the optimal configuration on speed and unbalance is discusse
d.