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Full Scale Span Load Distribution on a Tapered Wing with Split Flaps of Various Spans (1937)
NASA Technical Reports Server (NTRS) · leaf 13
N.A.C.A. Technical Note No. 591 Figure 3.- Half span tapered U.S.A.4o airfoil mounted in test position. 35.5 percent span flap.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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