Pierre-Yves

Thanks André. I used geometric progression for foil polar mesh and I reduced the number of polars and the discontinuity i away. PYves

Here is.

Hello All I started an analysis of a new glider. When I ask for a T2-VLM1 analysis of the wing only I get a discontinuity in the Cl vs Cd and VZ vs VX curves. After checking I saw that it comes from a discontinuity in the CD-Viscous calculation. Of course I already made the airfoils normalization and wings mesh re-initialization. What is going on? Thanks alezan