Full Scale Span Load Distribution on a Tapered Wing with Split Flaps of Various Spans (1937)
NASA Technical Reports Server (NTRS) · leaf 29
Fig* 19 N.A.C.A. Technical Note No- 591 … 100 20 40 60 80 Flap span in percentage of wing span* for a Effectiveness of added increments of flap Figure 19, span irfoil. 45 a £0 percent chord flap on a tapered U.S.A.
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