Wind tunnel data set with a wing at all angles of attack

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 settings are recorded in this data set. This data set should be valuable for the research on tailsitters, especially the impact of inverse flow on the tailsitters in the descending phase.