Supposed an air with density ρ and viscosity μ, is approaching a flat plate at uniform and
steady velocity u0. A thin boundary layer with thickness δ is developed when the air fl ows
over the flat plate as shown in FigQ4. It was determined that the boundary layer thickness is
a function of downstream distance x on the plate, approaching velocity, and fluid properties.
Use Buckingham Pi theorem to generate a dimensionless relationship for δ as a function of
the other parameters.
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