(a) Air is flowing Over a flat plate of 5 m long and 2.5 m Wide with a velocity of $4 \mathrm{~m} / \mathrm{s}$ at $15^{\circ} \mathrm{C}$. If $\rho=1.208 \mathrm{~kg} / \mathrm{m}^{3}$ and kinematic Viscosity $=1.47 \times 10^{-5} \mathrm{~m}^{2} / \mathrm{s}$, Calculate (i) length of plate Over which the boundary layer is laminar, and thickness of the boundary layer (Laminar) (ii) Shear stress at the location where the boundary layer ceases to be laminar and (iii) total drag force on the both sides on that Portion of plate where boundary layer is laminar.

Explanation

The length of the plate over which the boundary layer is laminar can be found using the Reynolds number. The thickness of the boundary layer can be found using the Blasius solution. The shear stress at the location where the boundary layer ceases to be laminar can be found using the Blasius solution. The total drag force on the both sides of the plate can be found using the drag equation.


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