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Development of the NACA slot-lip aileron (1935)
NASA Technical Reports Server (NTRS) · leaf 26
Fig. 11 N.A.C.A. 0.081 0.065 0.013 0.078 … -60 Aileron defleotion, 6a i degrees n- sass&r^ss ^e^oV^s gis.-sa^^^s^ gap 0.042c and slot width 0.066c.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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