Calculate the boundary-layer thickness at the exit of the


Air is entering a small 2D laminar flow wind tunnel at a speed of u1 = 10 m/s (L = 1 m, h = 0.2 m). Calculate the boundary-layer thickness at the exit of the wind tunnel at section 2. Also calculate the exit velocity u2.

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Mechanical Engineering: Calculate the boundary-layer thickness at the exit of the
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