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Design and Experimental Results for the S805 Airfoil
NREL
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Engineering
Experimental Result
100%
Design Result
100%
Airfoil
100%
Profile Drag
50%
Good Agreement
25%
Illustrates
25%
Horizontal Axis Wind Turbine
25%
Maximum Lift Coefficient
25%
Wind Tunnel Turbulence
25%
Drag Coefficient
25%