If I understand this right (and I MAY NOT):
- The leading edge should be rounded - nearly a half cylinder.
- Not the chord but the bisector of the angle between the upwind and downwind surfaces just behind the leading edge rounding should be angled at the TSR (at the end of the blade and scaled inversely with radius as you come toward the hub.)
- The trailing edge should be sharp and at a narrow angle.
- The bisector of the angle of the trailing edge should be at an angle of about 1/3 the TSR (again at the end of the blade and scaled inversely with radius.)
The idea is that:
- The leading edge must split the air even if it's not coming toward it at the bisector of the angle and must make it "attach" to both sides of the blade. You pay some air friction to increase the range of angles-of-attach over which the air attaches.
- The leading edge encounters the essentially undisturbed apparent wind and you want to split it evenly between the upper and lower surfaces.
- At the trailing edge you can rejoin the flows and form a jet going essentially the way the edge is pointed.
- The Betz ideal occurs when you slow the air to 1/3 its incoming speed, which dictates your trailing edge angle for a given operating TSR.
That doesn't take into account some other stuff (like pre-slowing of the air upwind of the blades by pressure from the blades' resistance propagating at sonic speeds, compensating for the energy left in the wind as spin and energy lost to surface drag, etc.) But I'm guessing this arrangement should be reasonably close to ideal.