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Full-scale Wind-tunnel to Determine a Satisfactory Location for a Service Pitot-static Tube on a Low-wing Monoplane (1936)

NASA Technical Reports Server (NTRS) · leaf 28

An illustration from Full-scale Wind-tunnel to Determine a Satisfactory Location for a Service Pitot-static Tube on a Low-wing Monoplane, 1936, leaf 28
Figure 21.- T0-31A mock-up. Wing: 7.38 (mean chord) by 45.75 ft., U.S.A. 45 section profile, elliptical plan form. Survey station: 0.036 sernispan inboard of wing tip.. Chord gg at survey station! 3 ft. 5 15/32 in. Pitot axis parallel to wing chord. Coordinates'* in per- £ centage of chord. to

NASA Technical Reports Server (NTRS)

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