Spectroscopy-based thrust sensor for high-speed gaseous flows

Measuring and testing – Vehicle chassis – Steering

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356315, G01M 1500

Patent

active

051780020

ABSTRACT:
A system and method for non-intrusively obtaining the thrust value of combustion by-products of a jet engine is disclosed herein. The system includes laser elements for inducing absorption for use in determining the axial velocity and density of the jet flow stream and elements for calculating the thrust value therefrom.

REFERENCES:
patent: 3852741 (1974-12-01), McDonald

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