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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 7

An illustration from The effects of full-span and partial-span split flaps on the aerodynamic characteristics of a tapered wing, 1934, leaf 7 — Fig. N.A.C.A. Technical Note No.505

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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