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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 8
Figs.2,3 N.A.C.A. Technical T«ote No. 505 … Figure 3.- The 0.15c constant- Figure 2-The 0.15c tapered- chord split flaps along chord split flaps along entire span of 5:1 tapered wing. entire span of 5:1 tempered wing.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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