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Preliminary Wind-Tunnel and Flight Tests of a Balanced Split Flap, Special Report (1934)
NASA Technical Reports Server (NTRS) · leaf 7
Fige. 3,3 N.A.C.A. L.E. … .40 34 8 IS 34 0 8 18 ct, , degrees oc, degress 3.- Lift, drag, and o.p. for wing with for wing with Figure Lift, drag, and o.p. Figure 3. unbalanced split flap. balanced split flap.NASA Technical Reports Server (NTRS)
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