Wind-tunnel tests on combinations of a wing with fixed auxiliary airfoils having various chords and profiles (1934)
NASA Technical Reports Server (NTRS) · leaf 4
ent e N.A.C.A. 22 auxiliary airfoil set at the optunnm angle for each 2S.0 percent t N.A.CJl. 22 anxUlary airfoil set at the optlmnm angle for each position. position. :6. I5r 5- Lod of trallfaig-«dge pojiUons for eqnal values of Cl^.x obtained with [a 7JS XiOcI of traUlng-edge positions for eqnal… … Loci of tialUng'edge positions for equal values of Z/J> at d-0.7 obtained with Xoci of tralling-edge positions for equal values of LID at Ctma obtained nitb a 7.6 percent c N-A.C.A. 0012 anxlliary airfoil set at the optimum angle for each a 7JS percent e N.A.OJL. 0012 auxlUary airfoil set at the…
NASA Technical Reports Server (NTRS)
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