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Wind Tunnel Tests on an Airfoil Equipped with a Split Flap and a Slot (1929)

NASA Technical Reports Server (NTRS) · leaf 10

An illustration from Wind Tunnel Tests on an Airfoil Equipped with a Split Flap and a Slot, 1929, leaf 10 — N.A.C.A. Teclinical Note No . 324 Fig.6 … Angle of attack Fig.6 Split flap down 30°.

NASA Technical Reports Server (NTRS)

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

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