|July 9, 2015, 15:33||
Super sonic CD nozzle in fluent 16.1
Join Date: Jul 2015
Posts: 3Rep Power: 2
I am a beginner in Ansys , trying to design a classic case of 2D Supersonic CD nozzle with exit mach number 3.0 with an ambient pressure at exit .
But flow decelerates after throat.
I think my definition of BC are incorrect (I applied massflow at inlet , walls and pressure oulet BC).
If you have any suggest please share.
or if you know of any similar model to take reference from please share.
Since i believe this is a very generic case , should be easy to model .but still i am not able to model it.
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