ORIGINAL: BMatthews
Close N1 but it's not thicker. Profili shows them both at 16% but the 8037 has 2.7% camber vs the 8036's 1.85%. But the effect is still what you want... a delayed stall at the tip. A form of aerodynamic washout.
Hi guys,
I too am looking for suitable airfoils for a scratch-design and I see the Selig sections mentioned often. But I have a question about the amount of washout used.... so with a root chord of 15" (& an S8036 'foil) and a 7" tip chord (& an S8037 'foil) - this seems very similar to N1EDMs

- does anyone have any idea how much washout I should add?
(Design is based on a lates '30s racer, 71" span and hopefully around 12lb, but I'm not interested in the speed, just a stable, predictable flyer).
Any help &/or advice would be much appreciated!