to get a numerical result for laminar flow karman assumed that the vel
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To get a numerical result for laminar flow, Kármán assumed that the velocityprofiles had anapproximately parabolic shape u(x, y) \approx U\left(\frac{2 y}{\delta}-\frac{y^{2}}{\delta^{2}}\right) \quad 0 \leq y \leq \delta(x)