Abstract

This work presents a hybrid (experimental-computational) application for improving the vibration behavior of structural components using a lightweight multilayer composite. The vibration behavior of a flat steel plate has been improved by the gluing of a lightweight composite formed by a core of polyurethane foam and two paper mats placed on its faces. This composite enables the natural frequencies to be increased and the modal density of the plate to be reduced, moving about the natural frequencies of the plate out of excitation range, thereby improving the vibration behavior of the plate. A specific experimental model for measuring the Operating Deflection Shape (ODS) has been developed, which enables an evaluation of the goodness of the natural frequencies obtained with the computational model simulated by the finite element method (FEM). The model of composite + flat steel plate determined by FEM was used to conduct parametric study, and the most influential factors for 1st, 2nd and 3rd mode were identified using a multifactor analysis of variance (Multifactor-ANOVA). The presented results can be easily particularized for other cases, as it may be used in cycles of continuous improvement as well as in the product development at the material, piece, and complete-system levels.

Highlights

  • The vibration behavior of a structural panel is an important factor in the operation of a machine or structure

  • Experimental modal analysis (EMA) is a technique that enables the determination of the resonances of a machine, identification of its modal parameters, and prediction of its vibration behavior [1]

  • The main interest is not to measure the eigenmodes, but the Operating Deflection Shape (ODS) and the resonance frequencies. It differs from investigations where the vibrational behaviors of thin steel sheets have been studied in that this work presents a composite computational model simulated by the finite element method (FEM), this model was used to conduct parametric study, and the most influential factors for 1st, 2nd and 3rd mode were identified using an analysis of variance (ANOVA) multifactor analysis

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Summary

Introduction

The vibration behavior of a structural panel is an important factor in the operation of a machine or structure. The main interest is not to measure the eigenmodes, but the ODSs and the resonance frequencies It differs from investigations where the vibrational behaviors of thin steel sheets have been studied in that this work presents a composite computational model simulated by the finite element method (FEM), this model was used to conduct parametric study, and the most influential factors for 1st, 2nd and 3rd mode were identified using an ANOVA multifactor analysis. This studied composite formed by a core of polyurethane foam differs from investigations where acoustical absorption is the main function of this type of composite [44]. OSD measurements have considered other types of structures and materials [4,5,6,7,8,9,10,11,12,13,14,15,16,17,18,19,20,21], or boundary conditions [45,46,47,48]

Methodological Approach
Samples
Experimental Test
Computational Study
Results and Discussion
ODS Experimental Measurements
FEM: Modal Analysis
Step 3
D: Adhesive
C: Outer Layers
Conclusions

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