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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 10

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 10 — NACA RM L50L04a 10 Chordwlse position vo LA -=* rA eg H o 6 , ‘lusTOfjjaoo ojnssaaa

NASA Technical Reports Server (NTRS)

Internet Archive · NASA Technical Reports · Public domain (US government work). Free to use for anything.

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