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The aerodynamic characteristics of a model wing having a split flap deflected downward and moved to the rear (1932)
NASA Technical Reports Server (NTRS) · leaf 10
I.A.O.A.Teolmioal lots 10.433 rigi. 4 & 5 fig.4 The 20 per oeut o flap hinged, at Fig.5 Tta6 30 par oent c flap hinged at 100 per oent o 70 pax cent cNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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