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 22
3 1 N.A.C.A. Technical Note No.659 Fig.5 … Aileron deflection, 6a , deg\ figure 5.- Rolling-moment and yawing-moment coefficients of plain ailerons on the full-span slotted flap of an N.A.C.A. 2303.2 rectangular wins of aspect ratio 6. (a) a = 0% (b)oc - 12°
NASA Technical Reports Server (NTRS)
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