I have an intake geometry which has two air inlets.I am specifying Pressure inlet as the boundary condition for both inlets.

The problem is that, the static pressure developed after the converged solution at the two inlets is different eventhough the total pressure specified in the Boundary conditions panel for both the inlets is the same assuming that the initial velocity at both the inlets has to be zero.

Is there any other way to specify the different boundary conditions for two different inlets.

Regards, Parag

You can specify different total pressure(and temperature). In your final result the velocity at the two inlets are not the same(and not zero, otherwise it is not inlet), that is why the static pressure is different.