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Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 43 and 63 (1931)
NASA Technical Reports Server (NTRS) · leaf 38
N.A..C.A. technical Uote sro.591 Pig. 6 … -4° 0*^ 4° 8° 12° 16° 20° 24° 2^ Angle of attack for infinite aspect ratio, Pig.6 lift CTorves for N.A.C.A.48 series airfoils.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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