Flow measurement device utilizing force transducers

Measuring and testing – Wind tunnel: aerodynamic wing and propeller study

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73180, 73188, G01C 2100, G01M 900

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active

047350857

ABSTRACT:
A missile-shaped body is calibrated to determine characteristic influence coefficients. Thereafter, the body is positioned in a flow field where normal forces and pitch moments are measured. Due to the fact that influence coefficients are predetermined as a result of calibration, the force and moment measurements are used to solve equations for flow field angularity.

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