Of so-called Nenadovich biplane or tandem wing configuration, the tandem-mounted wings providing a continuous slot effect and offering exceptional center of gravity range.
Relative angle of attack between the upstream and downstream airfoils (δ = α w α p ), where each angle of attack is taken with respect to the free stream. The decalage is therefore positive if the forewing incidence is greater than that of the rearwing or negative if the converse is true.
Positive decalage results in greater lift from the upper wing than the lower wing, the difference increasing with the amount of decalage (angle difference between the upper and lower wings chords)
In a survey of representative biplanes, real-life design decalage is typically zero, with both wings having equal incidence. A notable exception is the Stearman PT-17, which has 4° of incidence in the lower wing, and 3° in the upper wing. Considered from an aerodynamic perspective, it is desirable to have the forward-most wing stall first, which will induce a pitch-down moment, aiding in stall recovery. Biplane designers may use incidence to control stalling behavior, but may also use airfoil selection or other means to accomplish correct behavior.
For me, is seems the older dual-wing configurations is more of "STOL" capacity than speed.. even if such configuration give possibility for thinner airfoils, and less wingspan and smaller plane (aka speed and then quicker maneuverability eg.). And that the CG point get easier eg. by loads, so isnt as necessary to place it at actual point.
By some theories though, its mentioned that the room between for & aft "wings" can help less drag, and in subsonic we can today see lot of plane designs with a tandem systems, even if is just canards (who also is a tandem-wing versions)