Full-scale Wind-tunnel to Determine a Satisfactory Location for a Service Pitot-static Tube on a Low-wing Monoplane
This NACA technical report from 1936 presents full-scale wind-tunnel tests for placing a pitot-static tube on a low-wing monoplane, issued by the National Advisory Committee for Aeronautics for aeronautical engineers and researchers. Its pictures are plain engineering graphics: an airfoil profile beside a grid of pressure-coefficient contour lines and a photograph of a tapered airfoil model mounted in a wind tunnel, giving designers a clear, measured reference for airfoil cross-sections and technical diagram layout.
