Wind-tunnel tests on combinations of a wing with fixed auxiliary airfoils having various chords and profiles (1934)
NASA Technical Reports Server (NTRS) · leaf 10
ng a dual increase in (B) Anx. T.E. 11.5 percent abead of L.E., 14.0 percent above obord, {"V. the range of possible flight angles. Tiaoax 19.—Oliaracterbtlcs -with Olark T, 14.fi percent chord anxfltary. 6. The air load on the 14.5 percent symmetrical auxiliary airfoil was about one fifth the… … Cj^ -for entire wing Research Comparing Lateral Control Devices, Particularly (A) N.A.O-i. OOia, T.E. 11.6 percent ahead of L.E., 14.0 percent above chord. at High Angles of Attack. X. Various Control Devices (B) NJI.OJL 22, Tj;. 18.2 percent ahead of L.E., 12.0 percent above chord. on a Wing with…
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