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Wind-tunnel of three lateral-control devices in combination with a full-span slotted flap on an NACA 23012 airfoil (1938)
NASA Technical Reports Server (NTRS) · leaf 18
N.A.C.A.Technical Note No. 659 … Aileron deflect ion, 6a ,deg. Figure 3.- Rolling-moment and yawingxmoment coefficients of slot-lip ail- erons on an N.A.C.A.23012 rectangular wing- of aspect ratio 6 with full -span slotted flap. (a)or - 0 , (b)cC = IE*.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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