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January 20, 2010, 07:39 |
Simulations at different AoA
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#1 |
New Member
Join Date: Sep 2009
Posts: 27
Rep Power: 16 |
Hi,
I am trying to find out the change of lift coefficient with respect to AoA of an airfoil. To do this I run the same case but at different Aoa in fluent. All cases start from scratch and iterate till converge. Today I heard from my friend that I could have run a single case till converge, change the AoA, then continue running that case till converge for new AoA. Will the results be identical and more accurate? This will greatly save a huge amount of time. Thank you. |
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