Piotrsko
Master member
All airfoils require some sort of angle of attack device to generate lift, symmetric ones need couple degrees more possibly because the flat bottom that increases pressure is changed into a streamlined surface with a negative lift coefficient. Paper napkin engineering, could be wrong. Been so long since I built a wing with washout, I had to think about what it was. Washout should only affect tip stalls which can cause terminal death dive into the dirt, typically the stalled wing tip impacting first. On reflex, if the wing is making lift, the reflex is causing some drag. On a swept wing, that drag is typically behind the CG even if it has full trailing edge surfaces. Same as a straight wing, only less stabilizing effect because it's not as far from the CG. CANARDS are a whole different animal because the lifting surfaces aren't anywhere near the CG.