Air assumes steady, incompressible, and inviscid flows through the tunnel as indicated, where the velocity at section 1 is 15 m/s. The streamlines at section 1 are straight. A water manometer is attached to the tunnel via a wall pressure tap. Consider the tunnel to be 2D, and the diameter of the cylinder is 0.5 m. Ignore any hydrostatic (elevation) changes in the air. Calculate the gauge pressures:
a) at the stagnation point on the cylinder, and
b) at the point indicated on the streamline at section 2, the same cross section as the center of the cylinder.