Articles | Volume 11, issue 4
https://doi.org/10.5194/wes-11-1123-2026
https://doi.org/10.5194/wes-11-1123-2026
Data description article
 | 
08 Apr 2026
Data description article |  | 08 Apr 2026

An open database of high-fidelity, multi-Reynolds airfoil polars for wind turbine blade design

Francesco Papi, Pier Francesco Melani, and Alessandro Bianchini

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Revised manuscript under review for WES
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Cited articles

Abbott, I. H., Von Doenhoff, A. E., and Stivers, L.: Summary of Airfoil Data, National Advisory Committee for Aeronautics, https://ntrs.nasa.gov/citations/19930090976 (last access: 12 September 2025), 1945. 
U.S. Department of Energy: Airfoils, Where the Turbine Meets the Wind: https://www.energy.gov/eere/wind/articles/airfoils-where-turbine-meets-wind, last access: 23 October 2025. 
Andres, B.: COORDINATES AND CALCULATIONS FOR THE FFA-Wl-xxx, FFA-W2-xxx AND FFA-W3-xxx SERIES OF AIRFOILS FOR HORIZONTAL AXIS WIND TURBINES, Aeronautical Research Institute of Sweden, https://wind.nrel.gov/airfoils/Documents/FFA TN 1990-15 v.1-2 c.1.pdf (last access: 8 June 2020), 1990. 
Ansys Inc.: Ansys Fluent R24.2 User Guide – Section 36.13, Performing Time-Dependent Calculations, https://ansyshelp.ansys.com/public//Views/Secured/corp/v242/en/flu_ug/flu_ug_sec_solve_calc_time.html?utm_source (last access: 18 February 2026), 2024. 
Bak, C., Andersen, P. B., Madsen, H. A., Gaunaa, M., Fuglsang, P., and Bove, S.: Design and verification of airfoils resistant to surface contamination and turbulence intensity, in: Collect. Tech. Pap. AIAA Appl. Aerodyn. Conf., 26th Applied Aerodynamics Conference, Collect. Tech. Pap. AIAA Appl. Aerodyn. Conf., https://doi.org/10.2514/6.2008-7050, 2008. 
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This paper presents an open-access database of aerodynamic polars for a wide range of airfoils, relevant for wind turbine design and simulation. It includes lift, drag, and moment coefficients for multiple Reynolds and Mach numbers. Coefficients are computed with computational fluid dynamics for fully turbulent and free transition boundary layers, as well as a blend of the two. Beyond-stall extrapolation models are calibrated via a number of high-fidelity calculations at various angles of attack in separated flow.
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