Comparison of the transition location on the forward swept laminar wing

Comparison of the transition location on the forward swept laminar wing
Comparison of the transition location from the simulation (left and right) and the TSP measurement in the wind tunnel on the forward swept laminar wing. The transition location can be read from the clear increase in skin friction coefficient cf in the simulation and the change in the measured light intensity in the experiment. TSP measurement by the Institute of Aerodynamics and Flow Technology, Department of Experimental Methods