Consider a simple channel mesh, with inlet, wall and pressure BCs. All the
nodes at the exit are counted as pressure nodes, but the ones on the walls of
the exit plane are not counted as wall nodes. Therefore at the exit plane wall
velocities can not be equated to zero.
Original issue reported on code.google.com by cuneytsert on 24 Oct 2012 at 10:47
Original issue reported on code.google.com by
cuneytsert
on 24 Oct 2012 at 10:47