The illustration above is a cross section of a radiused steel valve seat insert showing typical issues where the insert transitions into the port wall, and where the top of the insert transitions to the chamber roof.
You can see at the transition from insert bottom to the port walls an overhang or underhang (or both) can occur leaving a sharp edge or uneven transition.
At the top of the insert, it is very typical to see a slight recession between the top of the insert and the combustion chamber roof (not to be confused with "valve seat recession"). I will not address this particular issue here, but only say that I have found only negative flow results in blending this area. Also, if this edge is very sharp, it may be wise to blend it, around the exhaust valve at least, for high compression or power adder applications to reduce the risk of predetonation.