hi friends i m simulating ejector flow, the nozzle is not collinear with secondary inlet. i want to simulate the no-load condition i,e secondary mass is zero and the secondary inlet becomes wall. in applying boundary condition there is one problem, one line is continuing from the secondary inlet to nozzle exit. that line when i give boundary condition up to nozzle inlet as wall and after that it is inside the domain so i have declared it as interior. when i declare like that error is coming can aby body tell some solution to the problem

[goami]

split that edge near the secondary inlet and specify accordingly........