Hi–I am currently trying to validate a simple reference wing in Simscale (https://www.simscale.com/workbench/?pid=3264969919978812504#tab_0-0).
When I input the wing geometry with the angle of attack as part of the geometry, my results are close to those from other techniques (VLM, 3D panel methods), as well as reference texts. However, if I mesh the wing with a 0 deg AoA and try to impose the AoA at the inlet boundary by changing the flow vector, my results are not close.
I believe I may have a meshing issue, or a lack of understanding of the inlet flow boundary conditions.
Any help will be appreciated!