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Full-scale Wind-tunnel and Flight Tests of a Fairchild 22 Airplane Equipped with a Fowler Flap (1936)
NASA Technical Reports Server (NTRS) · leaf 24
Fig. 9a N.A.C.I. Technioal Note lo. 578 Figure 9a.- Aerodynamic characteristics of Fairohild-23 airplane with 30-peroent Fowler flap. Flap retracted. Propeller and horizontal tail surfaoes removed. Results oorrected for tunnel effects. Test velocity, approximately 59 m.p.h.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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