| 000 | 03627nam a2200253Ia 4500 | ||
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| 003 | MX-MdCICY | ||
| 005 | 20250625162427.0 | ||
| 040 | _cCICY | ||
| 090 | _aB-19260 | ||
| 245 | 1 | 0 | _aArtificial neural networks and phenomenological degradation models for fatigue damage tracking and life prediction in laser induced graphene interlayered fiberglass composites |
| 490 | 0 | _vSmart Materials and structures, 30(8), p.085010, 2021 | |
| 520 | 3 | _aThe mechanical properties of fiber reinforced polymer matrix composites are known to gradually deteriorate as fatigue damage accumulates under cyclic loading conditions. While the steady degradation in elastic stiffness throughout fatigue life is a well-established and studied concept, it remains difficult to continuously monitor such structural changes during the service life of many dynamic engineering systems where composite materials are subjected to random and unexpected loading conditions. Recently, laser induced graphene (LIG)has been demonstrated to be a reliable, in-situ strain sensing and damage detection component in fiberglass composites under both quasi-static and dynamic loading conditions. This work investigates the potential of exploiting the piezoresistive properties of LIG interlayered fiberglass composites in order to formulate cumulative damage parameters and predict both damage progression and fatigue life using artificial neural networks (ANNs)and conventional phenomenological models. The LIG interlayered fiberglass composites are subjected to tension-tension fatigue loading, while changes in their elastic stiffness and electrical resistance are monitored through passive measurements. Damage parameters that are defined according to changes in electrical resistance are found to be capable of accurately describing damage progression in LIG interlayered fiberglass composites throughout fatigue life, as they display similar trends to those based on changes in elastic stiffness. These damage parameters are then exploited for predicting the fatigue life and future damage state of fiberglass composites using both trained ANNs and phenomenological degradation and accumulation models in both specimen-to-specimen and cycle-to-cycle schemes. When used in a specimen-to-specimen scheme, the predictions of a two-layer Bayesian regularized ANN with 40 neurons in each layer are found to be at least 60 percent more accurate than those of phenomenological degradation models, displaying R2 values greater than 0.98 and root mean square error (RMSE)values smaller than 10?3. A two-layer Bayesian regularized ANN with 25 neurons in each layer is also found to yield accurate predictions when used in a cycle-to-cycle scheme, displaying R2 values greater than 0.99 and RMSE values smaller than 2 × 10?4 once more than 30 percent of the initial measurements are used as inputs. The final results confirm that piezoresistive LIG interlayers are a promising tool for achieving accurate and continuous fatigue life predictions in multifunctional composite structures, specifically when coupled with machine learning algorithms such as ANNs. | |
| 650 | 1 | 4 | _aLASER INDUCED GRAPHENE |
| 650 | 1 | 4 | _aFIBERGLASS COMPOSITES |
| 650 | 1 | 4 | _aFATIGUE LIFE PROGNOSIS |
| 650 | 1 | 4 | _aARTIFICIAL NEURAL NETWORKS |
| 650 | 1 | 4 | _aPHENOMENOLOGICAL MODELS |
| 700 | 1 | 2 | _aNasser, J. |
| 700 | 1 | 2 | _aGroo, L. |
| 700 | 1 | 2 | _aSodano, H. |
| 856 | 4 | 0 |
_uhttps://drive.google.com/file/d/1431kNbF7Yy-F_HACOHaMN4AkyMXDlRbb/view?usp=drivesdk _zPara ver el documento ingresa a Google con tu cuenta: @cicy.edu.mx |
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