I've designed a series of airfoils for small WTs since I was not satisfied by the existing ones.
I've made also a machine layout with them ending up in a conservative cp=0.450 of the rotor (TSR of only 6!).
It's an xfoil-calc.
Critical comments welcome.
Discuss acquisition, use, and manipulation of airfoil data.
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- Location: Bolzano/Bozen in Italy
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