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 15
-1 … Angle of attack, ct ,deg. Angle of attack, at, deg. Angle of attack, oL, deg\ Figure 8.-Lift and drag coeffi- Figure 10.-Lift and drag coeffi- Figure G.- Lift and drag coef- cients of 5:1 tapered to cients of rectangular ficients of rectan- uring with full-span 0.20Cy 5:1 m gular wing with…
NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
