In this paper, we study the local existence and uniqueness of weak shocks in steady supersonic flow past a wedge. We take the potential flow equation as the mathematical model to describe the compressible flow. It is known that in generic case such a problem admits two possible locations of the shock front, connecting the flow ahead of it and behind it, provided that the vertex angle of the wedge is less than a critical value. They can be distinguished as supersonic-supersonic shock and supersonic-subsonic shock(or transonic shock). Both these possible shocks satisfy the Rankine-Hugoniot conditions and entropy condition. In this paper we prove the local existence and uniqueness of weak shock front if the coming flow is under small disturbance. |