Boundary Conditions for aircraft engine in Fluent 6.3 -- CFD Online Discussion Forums

July 20, 2011, 01:05	Boundary Conditions for aircraft engine in Fluent 6.3	#1
Tareen New Member Join Date: Jul 2011 Posts: 2 Rep Power: 0	Dear Friend(s), I am working on my final semester undergraduate engineering project. I have to study some modifications in a jet engine. Please guide me what should be the appropriate boundary conditions for the: - Domain inlet - Engine intake - Engine exit - Domain exit - The domain boundaries perpendicular to the engine's intake and exhaust planes The engine has to operate at 37,000 ft and the flow going into the engine's intake is at Mach = 0.8

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