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Pressure-distribution measurements on a rectangular wing with a partial-span split flap in curved flight (1939)
NASA Technical Reports Server (NTRS) · leaf 13
2.00 … 1.00 . 30 . 60 . 40 . 20 0 . 20 . 40 .60 .80 1.00 1.00 .AO .60 .40 .30 0 .20 .40 .60 .60 1. Position along wins »ptn Position »lon% wing span Figure 3.- Spanwiw distribution of noraal-loroe owffloient for 6* pitoh and »arioup yaw nicies.NASA Technical Reports Server (NTRS)
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