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Full-scale Wind-tunnel and Flight Test of a Fairchild 22 Airplane Equipped with a Zap Flap and Zap Ailerons (1937)

NASA Technical Reports Server (NTRS) · leaf 27

An illustration from Full-scale Wind-tunnel and Flight Test of a Fairchild 22 Airplane Equipped with a Zap Flap and Zap Ailerons, 1937, leaf 27
Figure 14.- Velocity diagram for Fairchild 22 airplane with Zap wing. From full-ecale wind-tunnel data:wind velocity,57 m.p.h.; weight,1600 lb.; wing area,171 sq.ft.

NASA Technical Reports Server (NTRS)

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