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Fig. 4 | Advances in Aerodynamics

Fig. 4

From: Vortex model of plane turbulent air flows in channels

Fig. 4

Velocity profiles over the plate at different distances (D) from the leading edge. Circles (\(\bigcirc\)) are the experimental data [1]; solid red lines correspond to the distribution (28). Fitting parameters are a \(\lambda /\delta = 0.21,\;\beta = 0.1\); b \(\lambda /\delta = 0.085\), \(\beta = 0.27\)

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