Advances in Aerodynamics

Table 1 The values of the fitting parameters f and \(\sigma\)

From: Vortex model of plane turbulent air flows in channels

Re	1844	2013	2293	3285	4653	5731	14147	24428	41441
f	0.26	0.21	0.17	0.105	0.068	0.055	0.028	0.019	0.014
\(\sigma\)	0.995	0.975	0.96	0.938	0.945	0.95	0.972	0.9805	0.986

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