Added option to Snap Spar to Surface or airfoil. Added option to remove spar's internal 'X' stamp. The aspect ratio is automatically adjusted to meet the users root chord and panel length criteria. The lofted ribs can then be generated with the resulting thicknesses as calculated, or forced into an elliptical thickness transition from root to tip. Added support to force the leading edge angle to that of the local washout angle.
Lofted ribs can now have a different airfoil at each panel juncture position.
You can now define the number of ribs within a wing panel instead of the spacing. Added support to generate multiple lofted foam templates with auto template height to create flat top surface. You can now define the wing sweep by leading edge angle. Support added to insert a panel within existing panels while lofting ribs. If you already have spars defined, and then add extra ribs, CompuFoil will now auto-compute and adjust the spars' starting and ending rib positions.