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-   -   Boundary Conditions for aircraft engine in Fluent 6.3 (http://www.cfd-online.com/Forums/fluent/90750-boundary-conditions-aircraft-engine-fluent-6-3-a.html)

Tareen July 20, 2011 00:05

Boundary Conditions for aircraft engine in Fluent 6.3
 
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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