However, I can provide a description of the sets of standard flows superimposed to represent the flow around a rotating cylinder.

The sets of standard flows superimposed to represent the flow around a rotating cylinder are:

1. Uniform Flow:
- This flow represents the incoming flow velocity which is uniform and parallel to the cylinder axis.
- It is represented by a set of parallel streamlines.

2. Potential Flow:
- This flow represents the flow around a stationary cylinder.
- It is represented by a set of streamlines which are symmetric about the cylinder axis.

3. Vortex Flow:
- This flow represents the flow around a rotating cylinder.
- It is represented by a set of circular streamlines which are centered on the cylinder axis.
- The flow direction around the cylinder is clockwise on the top and anti-clockwise on the bottom.

4. Boundary Layer Flow:
- This flow represents the flow near the surface of the cylinder where the velocity is lower than that of the free stream.
- It is represented by a set of streamlines which are parallel to the cylinder surface.
- The thickness of the boundary layer increases as the distance from the leading edge of the cylinder increases.

5. Separation Flow:
- This flow represents the flow near the rear end of the cylinder where the boundary layer separates from the surface.
- It is represented by a set of streamlines which curve away from the surface of the cylinder.
- The separation point moves towards the front of the cylinder as the rotation speed increases.

Overall, these sets of standard flows help in understanding the complex flow pattern around a rotating cylinder and are useful in designing and optimizing engineering applications such as wind turbines, marine propellers, and aircraft wings.