Differential Pressures on a Pitot-venturi and a Pitot-static Nozzle over 360 Degrees Pitch and Yaw
This is a 1928 NACA technical report by the NASA Technical Reports Server collection, measuring differential pressures on two aircraft pitot nozzles, a Navy pitot-venturi and a Navy SQ-16 pitot-static nozzle, as they were turned through 360 degrees of pitch and yaw. The pages are engineering working drawings with dimensioned sections and photographs of the probes mounted on test stands, useful to a designer for precise, technical line drawing of tubular instrument parts with callouts and section views.
