Wednesday, 08 September 2010
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Clarkston Test Site
VAWT/AR key parameters
(variables unique to the AR are in
red
)
Rotor diameter/airfoil length ratio
Airfoil aspect ratio (length to width)
Airfoil planform (shape of lifting surface)
Airfoil cant angle
Dampener response
Rotor tilt/airfoil pitch ratio
Rotor tilt/airfoil AOA limits
Centrifugal tilt compensation