Now you got me on a little rant.
Okay I'm not that mad, but I've been reading silly stuff here.
222 blades are more compatible
concave front profile of the blade
stalls at low angle of attack
Woah guys, you can't pretend to know as much as you say you do when it comes to airfoil shapes. I sat through a lot of aerodynamics classes and I still don't know either. There's some kind of group-think going on here and you're all together agreeing with yourselves.
This is not an art that accepts a piece of this and a piece of that. "Flat bottoms" and "concave surfaces" are totally irrelevant to the big picture of a wind turbine. I have tried working through the math with actual airfoil data, using all the right corrections and factors and so and any time there is the slightest glimmer of a possibility that one airfoil can do better than another, I can look at the big picture, add one inch to the radius, and all of the supposed advantage vanishes!
Who can tell me the difference between these airfoil coefficient curves?
Okay you thought that was so simple? Which one is BETTER? Ha you may still think that's easy to answer but have you calculated the CL / CD ratios? You'd be very very surprised if you did!
Who can pick the right shape that corresponds with the data above?
No I can't either! (well I wouldn't know if I hadn't made the graphics myself)
Who can tell me which will do better on such-and-such a turbine?
I don't know either!
Stop convincing yourselves that there is some particular part of the shape that does any thing for you. That is not how it works.
You want some math to help convince you? Draw out to scale a NACA4412 airfoil and beside it draw a Clark Y. What is the maximum different in the profile shapes? On a 6-inch chord, the differences are less than 1/16 of an inch. I defy you to carve or lay-up fiberglass by hand at that level of accuracy.
What about smoothness?
Tip Shape?
Root edge blend?
Trailing edge sharpness?
Your workmanship will have a 10x bigger effect on blade performance over airfoil selection. The only way you can screw up airfoil selection is to ignore the point of zero-lift and adjust the basic incidence accordingly when aiming for a specific TSR. Other than that you can sand down a fence board for all it matters at this scale.