The Effect of Split Trailing-edge Wing Flaps on the Aerodynamic Characteristics of a Parasol Monoplane (1933)
NASA Technical Reports Server (NTRS) · leaf 12
Angle of attack of thrust axis, otj) degrees Figure 5-Lif t,drag,and pitching-moraent curves for the Fairchild Y-ZZ airplane with split trailing -edge wing flaps.Horizontal tail surfaces set 0° to the thrust axis. Corrected for wind-tunnel effects.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
