Apparatus for determining stagnation pressure, static pressure,

Measuring and testing – Test stand – For engine

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73212, G01M 1500

Patent

active

041921780

ABSTRACT:
An apparatus for measuring stagnation pressure and yaw angle as well as providing static pressure and pitch angle indications at any point in subsonic and supersonic elastic fluid streams. Determination of both the static and stagnation pressures at any selected point permits Mach number determination anywhere along the radial length of axial flow turbine blades. Such localized Mach number determinations permit close monitoring of blade performance in axial flow turbines.

REFERENCES:
patent: 2650497 (1953-09-01), Renwanz
patent: 3167952 (1965-02-01), Kitagawa
patent: 3699811 (1972-10-01), Maiden et al.

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