Purpose: To estimate effects on the maximum and post-stall performance when curvature is added to a thin wing.
Here I detail 2D simulations on a circular arc wing. It is infinitely thin (aka 'baffle' in FOAM-speak), and the Reynolds number is 1.3 million.
Here I detail 2D simulations on a circular arc wing. It is infinitely thin (aka 'baffle' in FOAM-speak), and the Reynolds number is 1.3 million.
The files used to create these simulations can be found on my Github page under Gmsh/Sail2D (Case: 'first', Mesh: 'arc').