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Pressure-distribution measurements on a tapered wing with a partial-span split flap in curved flight (1939)
NASA Technical Reports Server (NTRS) · leaf 11
1.00 . 80 .60 . 40 . 20 0 . 20 .40 .60 .80 1.00 1.00 .80 . 60 .40 . 20 0 .20 . 40 . 60 .80 1.00 Position along wing span Position along wing span I Figure 3.- Distribution of normal-force coefficients along span of wing; plfcob, 5°. iNASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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