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Pressure distribution over a Clark Y-H airfoil section with a split flap (1937)
NASA Technical Reports Server (NTRS) · leaf 7
N.A.C.A.Technical Note No.627 … -Pressure distribution on the ClarkY-H airfoil at various Figure Z angles of attack- Split flap neutral.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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