Wind Turbine Performance in Controlled Conditions: BEM Modeling and Comparison with Experimental Results

Table 2

Maximum thickness and camber and their respective locations on the unit-length chord of each blade section at three radial positions: root, midsection, and tip of the aerodynamic span.

	Root	Midsection	Tip
Maximum thickness	0.195	0.217	0.164
at	0.225	0.300	0.325
Maximum camber	0.0755	0.0406	0.0326
at	0.600	0.375	0.400