Inside Out Library · Explore
Experiments with suction-type wings (1935)
NASA Technical Reports Server (NTRS) · leaf 45
U.Ut U.Ut ->";. - Figure 20.- Results for flap IIa, lift, profile Figure 31.- for flap II a, drag, suction pressure, suction p»30 . volume (flap angle p-15°),for a see Figs. 4&5.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
More pictures from Experiments with suction-type wings
More like this
