Inside Out Library · Explore
A simple method for increasing the lift of airplane wings by means of flaps (1933)
NASA Technical Reports Server (NTRS) · leaf 10
Figs. 4c,5,6 K.A.C.A, Technical Memorandum Ho. 714 … 2.0 1,0 30° a, 20^^ 10"- 0 esp O s/t =.20 Cutaway wing + s/t =.28 Cutaway wing. Figaro 5,- Pressure distri- X s/t =.10 Flap deflected downward ■bution alaout A = Smooth wing smooth V7ing (hatched) and about wing with flap accord- Figure 6.- Lift values obtained from ing to figure 1(circle).…NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from A simple method for increasing the lift of airplane wings by means of flaps
More like this
