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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 7

An illustration from Pressure distributions over a retracted leading-edge slat on a 40 degree sweptback wing at Mach numbers up to 0.9, 1951, leaf 7 — a 7 Figure 2.- Lift characteristics of wing at various Mach numbers *au3TOTJjso 0 wn

NASA Technical Reports Server (NTRS)

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