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Boundary Conditions for aircraft engine in Fluent 6.3

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Old   July 20, 2011, 00:05
Post Boundary Conditions for aircraft engine in Fluent 6.3
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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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