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Effect of changing the mean camber of an airfoil section (1924)
NASA Technical Reports Server (NTRS) · leaf 31
Fig, 3 Angle of attack, i=cic+i' H'ig, 3 Effect of maximum camber o/c on the C^. Res\£Lts for Royer airfoils (S.T.Ae, I3A - 21A)NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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