Air flowing over a flat plate at \(5 \mathrm{~m} / \mathrm{s}\) has a friction
coefficient given as \(C_{f}=0.664(V x / \nu)^{-0.5}\), where \(x\) is the
location along the plate. Using EES (or other) software, determine the effect
of the location along the plate \((x)\) on the wall shear stress
\(\left(\tau_{w}\right)\). By varying \(x\) from \(0.01\) to \(1 \mathrm{~m}\), plot
the wall shear stress as a function of \(x\). Evaluate the air properties at
\(20^{\circ} \mathrm{C}\) and \(1 \mathrm{~atm}\).