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Engineering, 01.11.2019 04:31 joelpimentel

Consider a laminar boundary layer formed by air flowing over a flat plate at a free-stream velocity of 2 m/s. suppose at a certain streamwise location the local streamwisevelocity is measured to be 1.7 m/s at a height of 2 mm above the plate. assumingblasius solution applies, determine: (a) the local skin-friction coefficient () the wall shear stress (τw)(c) the friction velocity (u∗)

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Consider a laminar boundary layer formed by air flowing over a flat plate at a free-stream velocity...

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