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Search: Posts Made By: John222
Forum: FLUENT November 30, 2011, 11:00
Replies: 0
Views: 2,814
Posted By John222
NACA 4412 airfoil for Cd

The drag coefficient is negative at high angle of attacks!!

however at 0 angle of attack it seems to be OK.

the lift coefficient is acceptable and good at all AOA.

What is the problem.

I...
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