- document
- Tang, X. (author), Schulte, F. (author) abstract 2023
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Tang, J. (author), van Bussel, G.J.W. (author)A new high-lift aerofoil modification for the duct has been developed and will be experimentally tested in a small wind tunnel. Aerofoils for such wind tunnel ducts typically operate in the low Reynolds number range from 2 × 105 to 6 × 105. The effect of a duct and of rotor on power and pressure drop were considered separately in previous...abstract 2017