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Pressure distributions over a retracted leading-edge slat on a 40 degree sweptback wing at Mach numbers up to 0.9 (1951)
NASA Technical Reports Server (NTRS) · leaf 13
MCA KM L50L04a 13 Figure 4.- Pressure distribution about wing leading edge at various angles of attaok. M a 0.10. Flap on, (a) o . 4.4° •NASA Technical Reports Server (NTRS)
Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.
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