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Tapered wings, tip stalling, and preliminary results from tests of the stall-control flap (1937)
NASA Technical Reports Server (NTRS) · leaf 23
-24 -20 -16 -12 -8 -4 0 4 8 12 16 20 24 28 2 0 .2 .4 .6 .8 1.0 1.2 1.4 1.6 1.8 2.0 2.2 2.4 2.6 Angle of attack, ct,deg. Section lift coefficient ct Figure 5NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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