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Rayleigh damping parameters estimation using hammer impact tests
•Analysis of Lamb wave propagation due to very low energy impacts on composite plates.•Rayleigh damping parameters estimated from lamb wave characteristics.•Finite element model simulation of the impacts show a good agreement with the test results. Structural Health Monitoring (SHM) systems for aero...
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Published in: | Mechanical systems and signal processing 2020-01, Vol.135, p.106391, Article 106391 |
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Main Authors: | , |
Format: | Article |
Language: | English |
Subjects: | |
Citations: | Items that this one cites Items that cite this one |
Online Access: | Get full text |
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Summary: | •Analysis of Lamb wave propagation due to very low energy impacts on composite plates.•Rayleigh damping parameters estimated from lamb wave characteristics.•Finite element model simulation of the impacts show a good agreement with the test results.
Structural Health Monitoring (SHM) systems for aerospace applications are becoming more prevalent and its potential cost-benefit relation is rapidly improving as more structures that were traditionally made with metallic materials are gradually being replaced by composites.
To support these systems, simulations can play a crucial role; however, in the case of low energy impacts, the structural damping becomes a very significant element in the simulation. This damping is usually not well known, or is based in estimates with very low reliability. Therefore, in order to improve the reliability of these values this paper presents an attempt to estimate the Rayleigh damping parameters with the application of time-frequency analysis methods to transient signals, specifically, the reduced interference distribution.
These parameters are estimated based in the results of a large number of structural tests done in a square carbon-fiber reinforced plastic panel, and are then validated by correlation of an explicit Finite Element Method (FEM) simulation.
A discussion on how to apply the reduced interference distribution to the signals measured by piezoelectric sensors under an impact scenario and other possible usages of these results is also presented in this document. |
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ISSN: | 0888-3270 1096-1216 |
DOI: | 10.1016/j.ymssp.2019.106391 |