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#1 |
Member
Join Date: Sep 2010
Posts: 45
Rep Power: 15 ![]() |
Hi all, I am doing simulation for a transonic compressor using ANSYS CFX. I found the tip shock is not very clear compared to the NUMECA results. The total pressure ratio is thus lower than the correct one.
Does anyone know the problem here? I am using k-epsilo turbulence model and high-resolution scheme. Thank you firstly, BalanceChen |
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#2 |
Super Moderator
Glenn Horrocks
Join Date: Mar 2009
Location: Sydney, Australia
Posts: 17,816
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#3 |
Member
Join Date: Sep 2010
Posts: 45
Rep Power: 15 ![]() |
Thank you very much for replying. I am trying to improve the grid quality~
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