Vortex-induced vibrations of a circular cylinder placed in a uniform flow at Reynolds number 325 are investigated using a stabilized space-time finite element formulation. The Navier-Stokes equations for incompressible fluid flow are solved for a two-dimensional case along with the equations of motion of the cylinder that is mounted on lightly damped spring supports. The cylinder is allowed to vibrate, both in the in-line and in the cross-flow directions. Results of the computations are presented for various values of the structural frequency of the oscillator, including those that are sub and superharmonics of the vortex-shedding frequency for a stationary cylinder. In most of the cases, the trajectory of the cylinder corresponds to a Lissajou figure of 8. Lock-in is observed for a range of values of the structural frequency. Over a certain range of structural frequency (FJ, the vortex-shedding frequency of the oscillating cylinder does not match F s exactly; there is a slight detuning. This phenom.enon is referred to as soft-lock-in. Computations show that this detuning disappears when the mass of the cylinder is significantly larger than the mass of the surrounding fluid it displaces. A self-limiting nature of the oscillator with respect to cross-flow vibration amplitude is observed. It is believed that the detuning of the vortex-shedding frequency from the structural frequency is a mechanism of the oscillator to self-limit its vibration amplitude. The dependence of the unsteady solution on the spatial resolution of the finite element mesh is also investigated.