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May 31, 2017, 09:54 |
Help micro gas turbine jet simualtion
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#1 |
New Member
anonymous
Join Date: May 2017
Posts: 6
Rep Power: 8 |
Hello everyone
I have an issue with my CFD simulation.. I simulate flow out of a nozzle of a micro turbine. I use BC: Axis, pressure far field(the domain has a shape of an ellipt with a length of 50 times the nozzle diameter), walls and mass flow inlet. density based- coupled but the results are not very good....the velocity of the exhaust is very low (230 m/s) instead of 360 m/s (result got from experiments) please help me...I'm desperate |
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