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They seemed to have gone through the wide chord route that will mitigate the lack of density by also reducing blade's span (but sadly reduce the max sustainable camber).I wouldn't be surprised if their airfoil has an aft max thickness point and a flat upper surface since there is no gain to expect with varying the pitch (does not exclude aero washout obviously).
They seemed to have gone through the wide chord route that will mitigate the lack of density by also reducing blade's span (but sadly reduce the max sustainable camber).
I wouldn't be surprised if their airfoil has an aft max thickness point and a flat upper surface since there is no gain to expect with varying the pitch (does not exclude aero washout obviously).
