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Aerodynamic effects of a split flap on the spinning characteristics of a monoplane model (1934)
NASA Technical Reports Server (NTRS) · leaf 10
40 50 60 70 -10 0 10 a, degress degrees Figure 2.-Change in longitudinal-force coefficient (from faired Cx curves) "body axes,produced by adding split flaps. Coefficients with split flaps minus coefficients with, plain wing. Right spin.NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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