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Fig. 9 | Advances in Aerodynamics

Fig. 9

From: A species-transport model for circulation in a leading-edge vortex

Fig. 9

Predicted shear-layer velocity profile along the span versus experimental shear-layer velocity distribution (from 1/4 to 1/2 the span) for a \(Re=1000\) and b \(Re=2500\). The predicted values are identified by a solid line only for the spanwise region of interest and become a dot line to represent the projected values of the spanwise region between the root and 1/4 of the span. When normalized by the wing tip velocity, the shear-layer velocity profiles for both Reynolds numbers are similar, if not identical

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