Calculate the flow around the circular cylinder of Example 7 .4 using the vortex panel method of Example 7 .5.

Data from Example 7.4

Simulate viscous flow around a circular cylinder for Re = 10⁵ using the DVM and a source panel distribution on the cylinder’s surface.

Data from Example 7.5

Calculate the unsteady aerodynamic loads acting on a 2D rectangular cylinder submerged in a steady free stream U_∞ at zero angle of attack for various values of the side ratio and compare to the results presented in Norberg (1993).