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 20
Aileron deflection, 6a , deg. Figure 6.-Hinge-moment coefficients of plain ailerons on the full-span slot- ted flap of an N.A.C.A. 23012, rectangular wing of aspect ratio 6 (a)ot=0*,(b)c(=l2o.
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
