The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing (1934)
NASA Technical Reports Server (NTRS) · leaf 11
Figs. 7,8 N.A.C.A. Technical Note No. 505 … Angle of attack, degrees, cL Angle of attack, degrees, a Figure 8.- Split flaps with center Figure 7.- Split flaps with tip sections removed sections removed on 5:1 tapered wing. on 5:1 tapered wing.
NASA Technical Reports Server (NTRS)
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