\( \mathrm{A}\) small round object is tested in a 0.75 -m diameter wind tunnel.
The pressure is uniform across sections (D and (2). The upstream pressure is
\(30 \mathrm{mm} \mathrm{H}_{2} \mathrm{O}\) (gage), the downstream pressure is
\(15 \mathrm{mm} \mathrm{H}_{2} \mathrm{O}\) (gage), and the mean air speed is
\(12.5 \mathrm{m} / \mathrm{s}\). The velocity profile at section (2) is linear;
it varies from zero at the tunnel centerline to a maximum at the tunnel wall.
Calculate (a) the mass flow rate in the wind tunnel,
(b) the maximum velocity at section \((2),\) and \((\mathrm{c})\) the drag of the
object and its supporting vane. Neglect viscous resistance at the tunnel wall.