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-ba
This wind tunnel data set was collected at OJF in TU Delft. The aerodynamic forces and moments of a modified MH32 wing at all angles of attack for different flap deflections and 0%, 70% throttle setti
Outputs of the numerical simulation for "Clear-air Turbulence Upstream of a Hydraulic Jump Leading to a Helicopter Accident - A Large Eddy Simulation".
