Article ID Journal Published Year Pages File Type
11003619 Measurement 2018 30 Pages PDF
Abstract
Results of forced and free decay response tests carried out on different types of composite blades are presented and discussed. They demonstrate that the proposed vibration exciter provides the capacity to identify geometrical nonlinearities and their effects in all the cases investigated.
Keywords
Related Topics
Physical Sciences and Engineering Engineering Control and Systems Engineering
Preview
Measurement of nonlinear vibration response in aerospace composite blades using pulsed airflow excitation
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