Alexei Grigoriev, Victor Malyutin, Alexei Chizhov, Andrei Gubernatenko

DOI Number: N/A

Conference number: IFASD-2015-093

In this paper there is a description of the approach of the experimental definition of Elastic influence coefficients’ matrix (ECM) using a number of linear displacements sensors and automated system of load application. Using the definition of the ECM of the engine mounted on wing of the dynamically-scaled model of the passenger aircraft as an example, the key characteristics of its realization are shown, which allow to minimize the main methodological inaccuracies.

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In Categories: 2. IFASD 2015, Experimental Methods
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