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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 24

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 24 — Figure 11.- Scale effect on the minimum drag coefficient of the Fairchild 22 airplane with flaps up. Propeller and horizontal tail surfaces removed; results corrected for wind-tunnel effects.

NASA Technical Reports Server (NTRS)

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

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