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The Effect of Split Trailing-edge Wing Flaps on the Aerodynamic Characteristics of a Parasol Monoplane (1933)
NASA Technical Reports Server (NTRS) · leaf 13
N.A.C.A. Fig. 6 … -15 -10 -5 0 5 10 15 20 Angle of attack of thrust axis, , degrees Figure 6 - Lift,drag, and piiching-jnoinent curves for the Fairchild F-ZZ airplane with split trailing-edge wing flaps. Horizontal tail surfaces removed. 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.
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