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Wind-tunnel tests on combinations of a wing with fixed auxiliary airfoils having various chords and profiles (1934)
NASA Technical Reports Server (NTRS) · leaf 9
OMMITTBE FOR AERONAUTICS ZO 0 20 0 5 40 ^ •S 1.6 1.6 100 ^ 1.2 1.2 .8 1—4 40 32 3 16 24 40 3Z O 8 16 24 -8 cC, degrees ct, degrees (A} Anx. T.E. 11 J! percent ahead o{ L.E., 14.0 percent above chord, <-3H°> (A) Attt. TJE. 18 J percent ahead of LJB., 2J percent below chord, 3-0°. (B) Aoz. T.E. 19.3… … -8 O a 16 24 32 40 '-B O e 16 24 32 40 d, degrees d,degrees (A) Ani. TJ;. 18.0 percent ahead of L.E., 14.0 percent above chord, J"0°. ( XA) Am. T.B. 18.0 percent ahead of L.E., 11.0 percent above dicffd, a—2Jf. (B) Am. T.E. 11.6 percent ahead of L.E., 14.0 percent above diord, »=0°. FiauBE…NASA Technical Reports Server (NTRS)
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