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Search: Posts Made By: ktgfeel
Forum: FLUENT November 27, 2014, 09:42
Replies: 1
Views: 1,588
Posted By ktgfeel
Lift coefficient with my 2.5D airfoil model never matches the experimental data.

Hi all

I have a problem in simulating 2.5 d airfoil particularly in lift coefficient.

I'm doing fluent to simulate Airfoil naca 4412 in water-liquid medium.

I have following conditions.
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