The large de ection of an elastoplastic beam with prescribed moving and rotating end conditions is investigated to simulate its air-bending process. A nite difference model is developed and governing equations in terms of rotations of elements were derived. D ue to both geometrical and material non-linearities, only numerical solutions are obtained by using an iteration procedure. F our typical examples with various moving/rotating boundary conditions are shown by graphs. N umerical analyses also show the evolution of the plastic region and the effects of springback and loading path on the deformed pro les.