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The aerodynamic characteristics of six commonly used Airfoils over a large range of positive and negative angles of attack (1931)
NASA Technical Reports Server (NTRS) · leaf 7
-32° -24° -16° -8° ' 0° 8° 16° 34° 32° Angle of attack,a Iig.2 Airfoil,JLA.C.A. CYH. Reynold's ffumber 3,100,000. V.D.T. besta,^ and 641. Aspect ratio>6. Tunnel wall correction applied. Dates,3/31 and 7/31-NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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