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Pressure distribution over a Clark Y-H airfoil section with a split flap (1937)
NASA Technical Reports Server (NTRS) · leaf 9
Figrurei4.-Pressure distrlbu*- tion on the Clark Y-H airfoil at i varioxis angles of attack. .12 0.15 Cy, split flap deflected ?» Cn^-0.66 60',NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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