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Tests of N.A.C.A. airfoils in the variable-density wind tunnel Series 230. (1936)
NASA Technical Reports Server (NTRS) · leaf 9
■ … .2 .4 .6" .<? /0 1.2 /.4 £0 -8 -4 0 4 8 12 16 20 24 28 32 ~4 -2 . Angle, of attach, ot (degrees) Lift coefficient c,, 3 Figure 3.- N.A/1A. 23012 airfoilNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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