Cambered Airfoil Wing Not Giving Proper Results in FLOWUnsteady

[prem-tekkr]

Hello,

I’m running a simulation with a cambered airfoil wing in FLOWUnsteady, but I’m not getting the expected results. The lift and drag values seem off.

Does anyone have suggestions on how to configure the simulation properly for a cambered airfoil? Any tips on what might be causing the issue?

Thanks in advance for your help!