|June 6, 2011, 02:58||
Shock capture in CFX
Join Date: Sep 2010
Posts: 45Rep Power: 6
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,
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