Inside Out Library · Explore

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 5

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 5

NASA Technical Reports Server (NTRS)

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

More pictures from Pressure distributions over a retracted leading-edge slat on a 40 degree sweptback wing at Mach numbers up to 0.9

More like this