The effect of partial-span split flaps on the aerodynamic characteristics of a Clark Y wing (1933)
NASA Technical Reports Server (NTRS) · leaf 7
20 40 60 80 m 100 0 10 £0 30 40 0 Flap chord, percent wing chord Flap length, percent wing span. Figure 2.-Effect of chord of split flap Figure* 5.-Effect of partial-span split flaps on CLjjjax and on Cd at Cl on Cl max max
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
