Inside Out Library · Explore

Wind-tunnel Investigation of Ground Effect on Wings with Flaps (1939)

NASA Technical Reports Server (NTRS) · leaf 21

An illustration from Wind-tunnel Investigation of Ground Effect on Wings with Flaps, 1939, leaf 21
Figs.6,7 N.A.C. A. Technical Note No 705 … Angle of attack , o£ , deg\ Angle of attack, oi ,deg\ Figure 7.-Tapered wing-; Figure 6. - Rectangular wing. taper ratio, 5:1. Effect of ground proximity on aerodynamic characteristics of N.A.C.A. 23012. wing with full-span 0.20cw split flap.

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

More pictures from Wind-tunnel Investigation of Ground Effect on Wings with Flaps

More like this