Wind-tunnel investigation of rectangular and tapered NACA 23012 wings with plain ailerons and full-span split flaps (1938)
NASA Technical Reports Server (NTRS) · leaf 12
H.A.C.A. Technical Kote Ho. 661 rige. 1,8 … Figure l. - The rectangular S.A.C.A. 23012 wing with 0.15 e. by 0.60 b/2 plain ailerons and a full-span 0.20 cw split flap at 0.65 c, and 0.85 a. A o o .70 o. 6* Ll8 * n * to -30.00"■ < A- 60.00" 7Y 8 .90 3 a ^ 3 30.OO" 60.00" Figure 2. - The rectangular H.A.O.A. 23013 wing with 0.10 o_ by 1.0O b/2…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
