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Large-Scale Boundary-Layer Control Tests on Two Wings in the NACA 20-Foot Wind Tunnel, Special Report (1935)
NASA Technical Reports Server (NTRS) · leaf 28
fig, 18 … -12 -6 0 6 12 Id 24 30 36 42 Ang/e of attack, , degrees Figure 19.- Lift curves with and without control. Wing with split flap. Blower speed constant.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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