Fig. 5From: Enhancing CFD predictions in shape design problems by model and parameter space reductionThe temporal evolution of the lift coefficient from \(1~\hbox {s}\) to \(30~\hbox {s}\) for 9 different parameters, together with the mean (dashed). The angle of attack is fixed for all the airfoil profiles and it is equal to \(0^\circ \)Back to article page