Load distribution of a wing with finite span. If the load distribution on a finite-span wing is as shown, sketch the trailing vortex system, indicating the magnitude and direction of the trailing vortices. On the plane defined by the wing/wake and the direction of the free stream, can you come up with a graphical representation of the downwash/upwash created by this vortex system? -b 2 -b b 4 6/2 b Figure 1: Spanwise circulation distribution for problem 1. y