I will respond to your specific initial questions.
Firstly, when driving a turbine rotor with a motor, the dynamics are completely different. As with any "fan blade", the rotor will produce swirling vortexes and the wind thus generated will not be uniform in cross-section (big hole in middle) and will spread out do to pressure difference vs the adjacent atmosphereic conditions. The air behind the rotor is dead still and you are now accelerating it to full speed by inputting a known amount of electrical energy. This is NOT to say that different blade geometries ie taper, twist, profile, cord dimension won't require different electrical juice, just that to correlate the data is unlikely to determine which one works the best in reverse with the wind blowing to generate electric power.
Back to running a rotor in a wind, some of the key features of any blade configuration has to do with air that is wasted by throwing it off the tips and also creating vortexes behind and the friction caused by drag at the highest velocities which detract from the lift which produces power.
I am in the middle of an experiment using a 12inch bench model and an artificial wind source ( not perfected yet) capable of 30mph WS. I have created about a dozen different blade designs and configurations and have not drawn any conclusions yet, other than thick blades at the tip don't work.
Hugh Piggot claims in his tutorial that flat, untwisted, and non-tapered blades may not be "ultimate designs", but there is surprisingly little to gain for fixed pitch, stall regulated, variable rotation spedd turbines.
You only have to check out the Bergey XL-1 to reach that same conclusion:
from an older thread "This is the current Bergey XL.1 airfoil. No twist. No taper....
but they work!
"Constant pitch with a little bit of the trailing tip cut off."
http://www.otherpower.com/images/scimages/110/xl1_airfoil_profile.JPG
That said, it is difficult to model a design and then blow it up to full size.
One reason is simple geometry. The airfoil analysis programs like JavaFoil show performance as a function of RE#, but RE# linearly depends upon WS and cord width.
TSR determines AOA and is independant of WS, so if you have a TSR=6, then a 12 inch rotor tip will spin at the same speed in mph as a 12 foot rotor (but 12x rpm), BUT the cord width is only 1/12 to scale it properly.
So, if in a 15mph WS and the cord of a real rotor is 5 inches (like Bergey), RE# is 360,000 , but the 12" model only has RE# = 30,000 ( and it goes down from there at lower stations!).
BTW, here is an interesting link to model testing/modeling being done at Clarkson Univ upstate NY:
http://www.clarkson.edu/honors/research/papers/Rector-M.%20Curtis.doc
Their interest is similar to mine in that higher pitch angle, higher solidity resulting in lower TSR, can result in higher efficiency for low WS conditions such as 12mph avg WS. I can note that Hugh indicated this premise in his charts and equations, but drew an different conclusion for his ultimate design.
I am almost ready to fly a 10+ footer with two rotors and 6 blades. I will update my progress when I have some data to publish.
I have some photos listed in my profile including most recently the finished blades
Stew Corman from sunny Endicott