Figure 2 - (a) Graphical representation of trail aircraft with relation to lead aircraft at position for optimal induced drag reduction, -0.15 y/b and 0.1 z/b; (b) Wing loading of trail aircraft rectangular wing with NACA0012 wing profile, flying at standard atmospheric conditions (0 meters) 0.55 Mach with a lift coefficient of 0.55, of a homogeneous formation where both wings are separated by eight wingspans.
{}