Issue |
MATEC Web Conf.
Volume 211, 2018
The 14th International Conference on Vibration Engineering and Technology of Machinery (VETOMAC XIV)
|
|
---|---|---|
Article Number | 06001 | |
Number of page(s) | 6 | |
Section | SM: Structural Modifications: Modelling Predictions and Experimental Assessment | |
DOI | https://doi.org/10.1051/matecconf/201821106001 | |
Published online | 10 October 2018 |
On reducing uncertainty on the Elliptical Plane modal identification method
1
Department of Design and Engineering, Faculty of Science and Technology, Bournemouth University,
Poole House, Talbot Campus, Fern Barrow,
Poole
BH12 5BB,
United Kingdom
2
School of Engineering and Technology, University of Hertfordshire, College Lane Campus,
Hatfield
AL10 9AB,
United Kingdom
* Corresponding author: dmontalvao@bournemouth.ac.uk
The Elliptical Plane has been recently introduced as a modal identification method that uses an alternative plot of the receptance. The method uses the dissipated energy per cycle of vibration as a starting point. For lightly damped systems with conveniently spaced modes, it produces quite accurate results, especially when compared to the well-known method of the inverse. When represented in the Elliptical Plane, the shape of the receptance is elliptical near resonant frequencies. The modal damping factor can be determined from the angle of the ellipse’s major axis with the horizontal axis, whereas the real and imaginary parts of the modal constants can be determined from numerical curve-fitting (as in the method of the circle - Nyquist plot). However, the lack of points that can be used near the resonance (due to limitations in the frequency resolution, and effects from other modes near each resonance) and the fact that measurements are polluted by noise, bring uncertainty to the numerical curve-fitting. This paper aims at providing the first steps on the improvement of the quality of the modal identification of the receptance in the Elliptical Plane. The method and results are discussed with a multiple degree-of-freedom numerical example.
© The Authors, published by EDP Sciences, 2018
This is an Open Access article distributed under the terms of the Creative Commons Attribution License (http://creativecommons.org/licenses/by/4.0), which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.
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