Inside Out Library · Explore

Flight Tests of Retractable Ailerons on a Highly Tapered Wing (1939)

NASA Technical Reports Server (NTRS) · leaf 14

An illustration from Flight Tests of Retractable Ailerons on a Highly Tapered Wing, 1939, leaf 14
Air speed Figure 7.- Variation of angle of roll attained in 1 second with air ap*ed» Retractable h* ailerons fully deflected; modified Fairchild 22 airplane. ?

NASA Technical Reports Server (NTRS)

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

More pictures from Flight Tests of Retractable Ailerons on a Highly Tapered Wing

More like this