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Nacelle Boundary Conditions

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February 12, 2020, 08:58	Nacelle Boundary Conditions	#1
rumed New Member Rumed İmrak Join Date: Dec 2019 Posts: 2 Rep Power: 0	Hey everyone, I am trying to simulate an aircraft geometry in farfield with engine fan face and nozzle boundary conditions. The problem is that I can not be sure that I can give an additional inlet and outlet boundary conditions additional to MARKER_FAR. PS: I do not want to simulate inside of engine. I have inlet and outlet values for pressure and tempereture. If you have any experience or suggestion according to topic I would be happy to read. Thanks!

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inlet, nacelle, outlet, riemann, su2

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