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November 2, 2019, 12:02 |
Request to make suggestion about the result
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#1 |
New Member
Join Date: Feb 2016
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Hi everyone,
I am doing some analysis in ansys fluent to see the free surface effect on NACA 0012 airfoil section in multiphase open channel flow using SST k-omega turbulence model. I have calculated the total pressure on the free surface. Can anyone suggest whether the result i have find is ok or not? I have attached the pressure contour figure along NACA 0012 for Fr = 0.55. Thanks in advance. Regards Habib https://drive.google.com/file/d/1RBG...ew?usp=sharing |
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