Measurements of differential pressures on two Navy air-speed nozzles, consisting of Zahm-type pitot-venturi tube and SQ-16 two-pronged pitot-static tube, in tunnel air stream of fixed speed at various angles of pitch and yaw between 0 and ± 180 deg., show for range over - 20 to + 20 deg. pitch and yaw, indicated air speeds varying very slightly over 2 per cent for Zahm type and maximum of 5 per cent for SQ-16 type from calibrated speed at 0 deg.
Differential pressures on a pitot-venturi and a pitot-static nozzle over 360 deg. Pitch and yaw
Nat. Advisory Committee Aeronautics -- Report
1927
9 pages
11 Figs.
Report
English
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