| Literature DB >> 35160827 |
Ewelina Kosicka1, Aneta Krzyzak2, Mateusz Dorobek3, Marek Borowiec4.
Abstract
Forecasting is one of the cognitive methods based on empirical knowledge supported by appropriate modeling methods that give information about the way the relations between factors and how the phenomenon under study will develop in the future. In this article, a selection is made of a suitable architecture for a predictive model for a set of data obtained during testing of the properties of polymer composites with a matrix in the form of epoxy resin with trade name L285 (Havel Composites) with H285 MGS hardener (Havel Composites), and with the addition of the physical modifier noble alumina with mass percentages of 5%, 10%, 15%, 20% and 25% for the following grain sizes: F220, F240, F280, F320, F360, respectively. In order to select the optimal architecture for the predictive model, the results of the study were tested on five types of predictive model architectures results were tested on five types of prediction model architectures, with five-fold validation, including the mean square error (MSE) metric and R2 determined for Young's modulus (Et), maximum stress (σm), maximum strain (εm) and Shore D hardness (⁰Sh). Based on the values from the forecasts and the values from the empirical studies, it was found that in 63 cases the forecast should be considered very accurate (this represents 63% of the forecasts that were compared with the experimental results), while 15 forecasts can be described as accurate (15% of the forecasts that were compared with the experimental results). In 20 cases, the MPE value indicated the classification of the forecast as acceptable. As can be seen, only for two forecasts the MPE error takes values classifying them to unacceptable forecasts (2% of forecasts generated for verifiable cases based on experimental results).Entities:
Keywords: L-BFGS; composites; machine learning; modeling; neural networks
Year: 2022 PMID: 35160827 PMCID: PMC8838961 DOI: 10.3390/ma15030882
Source DB: PubMed Journal: Materials (Basel) ISSN: 1996-1944 Impact factor: 3.623
Figure 1Zwick Z5.0 TN ZwickLine testing machine.
Figure 2Dimensions of composite specimens for the tensile strength test (mm).
Figure 3Bareiss Shore/IRHD Digi Test II, FRT GmbH, Bergisch Gladbach.
MSE values obtained for five types of model architectures.
| Mse Values For Individual Data Sets | ||||
|---|---|---|---|---|
| Model | Hardness | Et | σm | εm |
| Decision Tree Regressor | 1.5596 | 6057.3994 | 26.0022 | 0.1032 |
| MLP Regressor | 1.4614 | 6259.9139 | 25.2744 | 0.1060 |
| Linear Regression | 1.4810 | 10761.3150 | 50.4864 | 0.1851 |
| SVR | 1.4686 | 25829.4423 | 48.8113 | 0.1326 |
| K-Neighbors Regressor | 1.5443 | 7146.3127 | 31.3305 | 0.1198 |
Figure 4Program code snippet responsible for testing some predictive model architectures.
Selected results of the coefficient of determination.
| Activation | Alpha | Hidden Layer Sizes | R2 Score | |
|---|---|---|---|---|
| 0 | logistic | 0.0001 | 23 | 0.329345321 |
| 1 | logistic | 0.0001 | 25 | 0.316109079 |
| 2 | logistic | 0.0001 | 19 | 0.313990104 |
| 3 | logistic | 0.001 | 25 | 0.312857918 |
| 4 | logistic | 0.0001 | 21 | 0.293111995 |
| 5 | logistic | 0.001 | 21 | 0.285338460 |
| 6 | logistic | 0.0001 | 17 | 0.269040464 |
| 7 | logistic | 0.001 | 19 | 0.263106927 |
| 8 | logistic | 0.001 | 23 | 0.242614750 |
| 9 | identity | 0.0001 | 23 | 0.229048600 |
| 10 | identity | 0.0001 | 13 | 0.226608287 |
| 11 | identity | 0.0001 | 9 | 0.225083033 |
| 12 | logistic | 0.001 | 17 | 0.223577093 |
| 13 | identity | 0.001 | 7 | 0.218035216 |
| 14 | identity | 0.001 | 5 | 0.212440871 |
| 15 | identity | 0.0001 | 25 | 0.203615714 |
| 16 | identity | 0.001 | 17 | 0.202399900 |
| 17 | identity | 0.001 | 19 | 0.198601455 |
| 18 | identity | 0.0001 | 17 | 0.196738083 |
| 19 | identity | 0.0001 | 5 | 0.196004000 |
| 20 | identity | 0.0001 | 7 | 0.188281408 |
Figure 5Code snippet generating parameters of the selected neural network.
ME and MPE error values derived from prediction values for Et, σm and εm.
| Et | σm | εm | Hardness | |||||
|---|---|---|---|---|---|---|---|---|
| Composition of The Composite | ME | MPE | ME | MPE | ME | MPE | ME | MPE |
| EA 220/5 | 13.93 | 0.60% | 1.97 | 4.09% | 0.11 | 4.90% | −0.55 | −0.68% |
| EA 220/10 | 41.40 | 1.84% | 3.46 | 6.84% | 0.16 | 6.63% | 0.33 | 0.39% |
| EA 220/15 | −11.82 | −0.49% | −1.37 | −3.20% | −0.08 | −4.10% | −1.88 | −2.32% |
| EA 220/20 | −8.40 | −0.32% | 2.08 | 4.46% | 0.26 | 12.29% | −0.36 | −0.45% |
| EA 220/25 | −23.13 | −0.84% | 0.19 | 0.40% | −0.01 | −0.40% | 0.28 | 0.34% |
| EA 240/5 | −21.78 | −0.91% | 0.90 | 1.52% | 0.21 | 7.73% | 1.18 | 1.43% |
| EA 240/10 | 9.72 | 0.39% | 2.81 | 4.82% | 0.16 | 5.82% | −0.10 | −0.12% |
| EA 240/15 | 21.17 | 0.83% | 2.56 | 4.78% | 0.16 | 6.46% | 0.03 | 0.03% |
| EA 240/20 | −8.19 | −0.31% | 3.17 | 6.31% | 0.17 | 8.23% | 0.52 | 0.62% |
| EA 240/25 | −37.17 | −1.44% | −2.27 | −5.92% | −0.03 | −2.05% | −0.05 | −0.06% |
| EA 280/5 | 33.63 | 1.34% | −1.12 | −2.29% | −0.14 | −7.04% | −0.68 | −0.83% |
| EA 280/10 | −92.36 | −3.88% | −1.82 | −3.65% | −0.05 | −2.15% | −0.13 | −0.15% |
| EA 280/15 | 38.43 | 1.53% | −3.05 | −6.28% | −0.26 | −12.56% | −0.20 | −0.24% |
| EA 280/20 | 24.49 | 0.97% | 0.72 | 1.70% | 0.03 | 1.95% | 0.19 | 0.23% |
| EA 280/25 | −1.65 | −0.06% | −2.29 | −5.63% | −0.08 | −5.24% | −0.12 | −0.15% |
| EA 320/5 | −14.67 | −0.63% | 2.11 | 3.98% | 0.11 | 4.62% | 0.69 | 0.82% |
| EA 320/10 | −12.92 | −0.52% | −0.04 | −0.07% | 0.00 | −0.05% | 0.25 | 0.29% |
| EA 320/15 | 2.56 | 0.10% | −1.48 | −2.62% | −0.15 | −6.46% | −0.19 | −0.22% |
| EA 320/20 | −47.68 | −1.83% | −2.42 | −4.33% | −0.15 | −6.36% | 0.09 | 0.11% |
| EA 320/25 | −21.90 | −0.84% | −2.30 | −6.23% | −0.07 | −5.18% | 0.20 | 0.24% |
| EA 360/5 | 9.27 | 0.40% | −3.91 | −8.40% | −0.20 | −9.15% | 0.74 | 0.89% |
| EA 360/10 | 0.99 | 0.04% | 1.94 | 3.11% | 0.10 | 3.37% | −0.31 | −0.37% |
| EA 360/15 | 66.16 | 2.70% | 0.90 | 1.45% | 0.04 | 1.43% | −0.05 | −0.07% |
| EA 360/20 | −10.27 | −0.40% | −0.45 | −0.84% | −0.08 | −3.36% | −0.70 | −0.85% |
| EA 360/25 | −29.81 | −1.07% | 3.97 | 7.65% | −0.13 | −6.25% | −0.33 | −0.39% |
Figure 6This 3D maps generated from the predicted values of hardness (a), Young’s modulus (Et) (b), ultimate tensile stress (σm) (c), and relative elongation (εm) (d).