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Pressure distribution over a Clark Y-H airfoil section with a split flap (1937)

NASA Technical Reports Server (NTRS) · leaf 8

An illustration from Pressure distribution over a Clark Y-H airfoil section with a split flap, 1937, leaf 8 — Figrure 3,-Pressure distribution on the Clark Y-H airfoil at ; ' J, various angles of attack. 0.15 aplit flap oq deflected 30'. « i

NASA Technical Reports Server (NTRS)

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