Data supporting the research of FFA-W3-211 experimental polars

The dataset includes experimental data for the FFA-W3-211 airfoil, with a chord of c= 0.6m, tested at the low-speed low turbulence tunnel at TU Delft. The experiment is carried out for static chord-based Reynolds numbers between 500.000 and 3.500.000, and dynamic Reynolds numbers of 500.000, 1.000.000 and 2.000.000. The force coefficients were acquired for the static and dynamic cases, using a turntable for the former and a linear actuator for the latter. Data is acquired via pressure taps and wake rake. The static and dynamic data are presented and processed as per the description in the publication.