Summary of the Blind Test Campaign to predict the High Reynolds number performance of DU00-W-210 airfoil

What is it about?

This paper presents a blind comparison of computational data against experimental results obtained in a wind tunnel test. The wind tunnel test was performed on a wind turbine blade airfoil simulating the conditions attained at the new multi-MW machines with high rotor dimensions. These conditions are expressed in the non-dimensional aerodynamic parameter called Reynolds number.

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