Evgeni G

Hi, I am new to XFLR5 and probably the problem is in my process and/or settings. What I get is an error when I try to perform XFLR Direct Analysis of AG35 airfoil. In Define Analysis my settings are the following: Analysis type: 1 Re: 80K Mach = 0.000 Ncrit=9 Trip Location top 1 Trip Location bot 1 In the left side my settings are: afla Sequence Start = -10 End = 10 delta/angle = 1 Viscous Init BL Store Opp The polars look weird to me, I am attaching a screenshot. Log File: xflr5 v6.56 AG35 T1_Re0.080_M0.00_N9.0...