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Search: Posts Made By: Aarib
Forum: FLUENT April 26, 2021, 22:10
Replies: 0
Views: 543
Posted By Aarib
Fluent giving correct values for Cd but incorrect values for Cl

I'm trying to simulate the flow over a 2D airfoil in Fluent. The solver is steady with k-omega SST model.

At different angles of attack, the value of Cd i get is always correct but value of CL is...
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