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The calculated effect of trailing-edge flaps on the take-off of flying boats (1934)
NASA Technical Reports Server (NTRS) · leaf 18
N.A.C.A. Technical Note No.510 Figs. 5,6 0 10 20 30 40 50 60 70 ■ 80 ■ 90 100 110 120 130 Speed, f.p.s. ... Figure 5.-Effect of flaps on the taKe-off resistance of seaplane B using a wing setting of G._6° . —- … 0 10 20 30 40 50 .60 70 80 90 100 110 120 130 Speed, f.p.s. ~'■ Figure—6r-Ef feet of flaps on 4ha_ taKe-pf f -j°eg-h34enGe-o-r~55aphane^A_ using -&rwing_^et-t-ing-xjf-~-4°. *NASA Technical Reports Server (NTRS)
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