Artificial Neural Network Modeling for Prediction of Welding Transverse Distortion in TIG Welding of Mild Steel ()
1. Introduction
Tungsten Inert Gas (TIG) welding remains a cornerstone fabrication process for medium-to-thick structural sections due to its exceptional arc stability and high-integrity joint formation [1] [2]. However, the localized thermal cycling inherent to the process generates non-uniform expansion and contraction, inevitably inducing transverse distortion that compromises dimensional accuracy, assembly tolerances, and structural service life [3] [4]. Conventional predictive approaches, including empirical regression models and simplified analytical formulations, frequently fail to capture the highly nonlinear thermo-mechanical interactions governing distortion in 10 mm mild steel plates [5]. These methods rely on rigid mathematical assumptions that oversimplify heat transfer dynamics and material phase transformations, resulting in inadequate forecasting precision for industrial fixture design and pre-weld process planning [6] [7].
Artificial Neural Networks (ANNs) circumvent these limitations by learning complex input-output mappings directly from experimental data without requiring explicit physical constitutive equations [8] [9]. Recent investigations have successfully deployed ANN architectures to predict weld bead geometry, penetration depth, and residual stress across various fusion welding processes [10]-[12]. Studies have specifically demonstrated ANN’s effectiveness in predicting weld quality parameters for TIG welded mild steel joints, including mechanical properties and bead characteristics [8] [13] [14]. Despite this progress, systematic validation of feedforward ANNs for transverse distortion prediction in 10 mm TIG-welded mild steel remains underexplored. Most existing studies either prioritize thinner sections, rely on simulated finite element datasets with limited experimental grounding, or omit rigorous statistical validation against unseen test conditions [15] [16]. Consequently, a robust, experimentally calibrated ANN framework tailored to the specific thermal and mechanical boundary conditions of thick-plate TIG welding is critically needed [17] [18].
This study directly addresses this gap by developing and rigorously validating a single-output feedforward ANN model dedicated to predicting transverse distortion in 10 mm ASTM A36 mild steel plates. A Central Composite experimental matrix spanning practical welding current, voltage, shielding gas flow rate, and welding speed ranges was designed to generate a high-fidelity dataset for model training and testing [19] [20] [13]. The ANN architecture undergoes systematic optimization and validation using regression analysis, mean squared error quantification, and error distribution mapping to ensure statistical reliability [5] [21]. Previous optimization studies on mild steel welds have successfully employed metaheuristic and multi-criteria decision-making approaches such as MOORA, AHP, Fuzzy C-Means, and Taguchi methods, demonstrating the viability of data-driven strategies for weld quality improvement [3] [22] [23]-[25]. Additionally, recent advances in predictive modeling have shown that ANN can effectively forecast weld droplet diameter, solidus temperature, and droplet temperature in gas metal arc welding, further supporting the applicability of neural networks to complex thermal phenomena [21]. By establishing a direct, experimentally verified correlation between process parameters and transverse distortion, this work delivers a computationally efficient predictive tool that reduces trial-and-error iterations and supports data-driven process optimization in structural welding applications [26]-[29].
2. Methodology
2.1. Material and Equipment
Plate 1 shows visible presence of distortion on mild steel plate sample from welding experiments. The base material, 10 mm thick ASTM A36 mild steel, was cut into plates measuring 300 mm in length and 150 mm in width. A single V-groove butt joint configuration with a 60˚ included angle and a 2 mm root gap was prepared for edge preparation. Welding was performed in autogenous mode for the root pass, followed by two subsequent filler passes using an ER70S-6 filler wire, resulting in a total of three passes. The process utilized Direct Current Electrode Negative (DCEN) polarity. The torch was maintained at a travel angle of 75˚ relative to the workpiece. To minimize excessive out-of-plane deformation while accommodating thermal expansion, the plates were rigidly clamped to a heavy steel backing fixture with a copper backing strip to ensure full root penetration and restrain the workpieces. TIG welding was conducted using a computerized GTAW system with high-purity argon (99.99%) serving as the shielding gas.
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Plate 1. 10 mm mild steel plate sample with visible distortion.
Post-weld transverse distortion measurements were conducted after the plates had completely cooled to room temperature, specifically 24 hours after welding, to eliminate any transient thermal expansion effects. Measurements were taken at three distinct locations along the mid-span of the weld length (at the center and 50 mm from both edges). At each location, three readings were recorded and averaged to represent the plate’s distortion. Initial coarse measurements were performed using calibrated digital micrometers, and these were subsequently cross-verified and combined with high-resolution optical profilometry scans at the same locations to maintain a measurement uncertainty of ±0.005 mm.
Four governing process parameters guided the experimental matrix: welding current (A), arc voltage (V), shielding gas flow rate (L/min), and welding speed (cm/min). A Face-Centered Central Composite Design (FCCD) variant was employed for the experimental matrix. The design comprised 16 factorial points (coded as ±1), 8 axial points located at the face centers (coded as α = ±1), and 6 center-point replicates (coded as 0) to estimate pure error and ensure design rotatability. This layout generated the 30 distinct experimental runs presented in Table 1, optimizing parameter space exploration while minimizing resource expenditure.
Table 1. Process parameters and their coded levels for CCD experimental design.
Parameter |
Unit |
Symbol |
Low (−1) |
High (+1) |
Current |
Amp |
A |
130 |
170 |
Voltage |
Volt |
V |
20 |
24 |
Gas flow rate |
L/min |
F |
19 |
25 |
Welding speed |
cm/min |
S |
6 |
10 |
2.2. ANN Architecture and Training Protocol
Figure 1. Schematic of the 4-10-1 feedforward ANN architecture for transverse distortion prediction.
A multilayer feedforward neural network presented in Figure 1 was developed to map the four input parameters to transverse distortion. The architecture comprises an input layer (4 neurons), a single hidden layer (10 neurons with hyperbolic tangent activation), and an output layer (1 neuron). The 4-10-1 ANN architecture was selected based on a systematic tuning process. The number of hidden neurons was determined using the heuristic formula
(where C is a constant between 1 and 10) and refined via trial-and-error to minimize the Mean Squared Error (MSE) on the validation set without causing overfitting, aligning with established neural network design principles [9].
To establish a baseline and quantify the advantage of the nonlinear mapping capability of the ANN, a simple Multiple Linear Regression (MLR) model was also developed using the same dataset. The MLR model yielded a significantly lower overall R2 of 0.784, confirming that the ANN architecture provides a substantial improvement in capturing the complex, nonlinear thermo-mechanical interactions of the welding process.
The Levenberg-Marquardt backpropagation algorithm was selected to ensure rapid convergence on the experimental dataset. Prior to training, min-max scaling normalized all input and output variables to the [0, 1] range, preventing gradient instability. The dataset was partitioned into training (70%), validation (15%), and testing (15%) subsets, preserving balanced parameter distributions across each split. Model training incorporated a maximum of 100 epochs, an early stopping patience of 6 epochs, and a target gradient threshold of 1 × 10−7. Random weight initialization employed a fixed seed (42) to guarantee reproducibility. All computational procedures were executed in MATLAB R2024b utilizing the Neural Network Toolbox.
3. Results and Discussion
3.1. Experimental Trends and Thermal Input Dynamics
Transverse distortion varied between 0.1729 mm and 0.4278 mm across the 30 experimental runs (Table 2). Peak distortion occurred at high current (170 A) and low welding speed (6 cm/min), consistent with elevated net heat input promoting asymmetric thermal expansion and contraction. Conversely, reduced distortion at high welding speed (10 cm/min) correlates with shorter exposure time and lower cumulative thermal strain. These baseline trends establish the physical context for ANN validation.
Table 2. Experimental matrix and measured transverse distortion for 30 CCD runs.
Run |
A: Current |
B: Voltage |
C: Gas Flow Rate |
D: Welding Speed |
Transverse |
|
Amp |
V |
L/min |
cm/min |
mm |
1 |
130 |
20 |
22 |
8 |
0.3619 |
2 |
170 |
20 |
22 |
8 |
0.3729 |
3 |
130 |
24 |
22 |
8 |
0.28 |
4 |
170 |
24 |
22 |
8 |
0.3844 |
5 |
150 |
22 |
19 |
6 |
0.3063 |
6 |
150 |
22 |
19 |
10 |
0.3756 |
7 |
150 |
22 |
25 |
6 |
0.3615 |
8 |
150 |
22 |
25 |
10 |
0.1729 |
9 |
130 |
22 |
19 |
8 |
0.2861 |
10 |
170 |
22 |
19 |
8 |
0.4221 |
11 |
130 |
22 |
25 |
8 |
0.3093 |
12 |
170 |
22 |
25 |
8 |
0.2621 |
13 |
150 |
20 |
22 |
6 |
0.3962 |
14 |
150 |
24 |
22 |
6 |
0.3082 |
15 |
150 |
20 |
22 |
10 |
0.2815 |
16 |
150 |
24 |
22 |
10 |
0.3112 |
17 |
130 |
22 |
22 |
6 |
0.3528 |
18 |
170 |
22 |
22 |
6 |
0.3547 |
19 |
130 |
22 |
22 |
10 |
0.2388 |
20 |
170 |
22 |
22 |
10 |
0.3516 |
21 |
150 |
20 |
19 |
8 |
0.4278 |
22 |
150 |
24 |
19 |
8 |
0.3063 |
23 |
150 |
20 |
25 |
8 |
0.2663 |
24 |
150 |
24 |
25 |
8 |
0.3268 |
25 |
150 |
22 |
22 |
8 |
0.3006 |
26 |
150 |
22 |
22 |
8 |
0.3036 |
27 |
150 |
22 |
22 |
8 |
0.32 |
28 |
170 |
20 |
25 |
10 |
0.211 |
29 |
170 |
20 |
25 |
6 |
0.3173 |
30 |
150 |
22 |
22 |
8 |
0.3055 |
3.2. ANN Training Dynamics and Convergence
The ANN model achieved optimal performance within 5 training epochs (Figure 2). The training state plot confirms gradient descent stabilization, with the final gradient (8.89 × 10−9) falling well below the convergence threshold (Figure 3). Validation checks triggered early stopping at epoch 3, preventing overfitting despite limited dataset size (Figure 4). The performance plot demonstrates consistent MSE reduction across training, validation, and test subsets, indicating stable optimization without memorization artifacts.
Figure 2. ANN training convergence plot for transverse distortion prediction (MSE vs. epoch).
Figure 3. Training state plot showing gradient, mu, and validation checks during ANN optimization.
Figure 4. Performance plot illustrating MSE progression across training, validation, and test datasets.
3.3. Predictive Accuracy and Experimental Validation
The ANN model predicted transverse distortion with high fidelity, yielding an overall R2 of 0.911 and a final MSE of 9.41 × 10−6 (Table 3). Run-by-run predictions alongside experimental measurements show a mean absolute error (MAE) of 0.018 mm, with 83% of predictions deviating by less than ±0.025 mm from experimental values. Regression analysis (Figure 5) confirms a linear correlation slope near unity and minimal intercept bias. The error histogram (Figure 6) reveals a Gaussian distribution centered at zero, with ±0.0061 mm encompassing the majority of residuals, confirming unbiased prediction behavior.
Table 3. Experimental versus ANN-predicted transverse distortion with absolute error analysis.
Run |
A: Current |
B: Voltage |
C: Gas Flow Rate |
D: Welding Speed |
Transverse Deformation |
|
Amp |
V |
L/Min |
cm/min |
Exp |
ANN |
Error |
1 |
130 |
20 |
22 |
8 |
0.3619 |
0.352063345 |
0.009836655 |
2 |
170 |
20 |
22 |
8 |
0.3729 |
0.365064386 |
0.007835614 |
3 |
130 |
24 |
22 |
8 |
0.28 |
0.265292427 |
0.014707573 |
4 |
170 |
24 |
22 |
8 |
0.3844 |
0.380881071 |
0.003518929 |
5 |
150 |
22 |
19 |
6 |
0.3063 |
0.30202395 |
0.00427605 |
6 |
150 |
22 |
19 |
10 |
0.3756 |
0.374092552 |
0.001507448 |
7 |
150 |
22 |
25 |
6 |
0.3615 |
0.395749276 |
−0.034249276 |
8 |
150 |
22 |
25 |
10 |
0.1729 |
0.178856198 |
−0.005956198 |
9 |
130 |
22 |
19 |
8 |
0.2861 |
0.282299249 |
0.003800751 |
10 |
170 |
22 |
19 |
8 |
0.4221 |
0.420026454 |
0.002073546 |
11 |
130 |
22 |
25 |
8 |
0.3093 |
0.372368449 |
−0.063068449 |
12 |
170 |
22 |
25 |
8 |
0.2621 |
0.286141748 |
−0.024041748 |
13 |
150 |
20 |
22 |
6 |
0.3962 |
0.389404845 |
0.006795155 |
14 |
150 |
24 |
22 |
6 |
0.3082 |
0.311733118 |
−0.003533118 |
15 |
150 |
20 |
22 |
10 |
0.2815 |
0.270403135 |
0.011096865 |
16 |
150 |
24 |
22 |
10 |
0.3112 |
0.306556668 |
0.004643332 |
17 |
130 |
22 |
22 |
6 |
0.3528 |
0.369502353 |
−0.016702353 |
18 |
170 |
22 |
22 |
6 |
0.3547 |
0.308034895 |
0.046665105 |
19 |
130 |
22 |
22 |
10 |
0.2388 |
0.203480859 |
0.035319141 |
20 |
170 |
22 |
22 |
10 |
0.3516 |
0.402379555 |
−0.050779555 |
21 |
150 |
20 |
19 |
8 |
0.4278 |
0.380123968 |
0.047676032 |
22 |
150 |
24 |
19 |
8 |
0.3063 |
0.300293184 |
0.006006816 |
23 |
150 |
20 |
25 |
8 |
0.2663 |
0.305162188 |
−0.038862188 |
24 |
150 |
24 |
25 |
8 |
0.3268 |
0.299596922 |
0.027203078 |
25 |
150 |
22 |
22 |
8 |
0.3006 |
0.298707157 |
0.001892843 |
26 |
150 |
22 |
22 |
8 |
0.3036 |
0.298707157 |
0.004892843 |
27 |
150 |
22 |
22 |
8 |
0.32 |
0.298707157 |
0.021292843 |
28 |
170 |
20 |
25 |
10 |
0.211 |
0.188031735 |
0.022968265 |
29 |
170 |
20 |
25 |
6 |
0.3173 |
0.332977411 |
−0.015677411 |
30 |
150 |
22 |
22 |
8 |
0.3055 |
0.298707157 |
0.006792843 |
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Figure 5. Regression plot comparing experimental versus ANN-predicted transverse distortion (R = 0.911).
Figure 6. Error histogram showing residuals concentrated near zero (±0.0061 mm), confirming unbiased ANN predictions.
3.4. Error Analysis and Process Regime Sensitivity
Prediction errors concentrated in parameter extremes. Run 11 (130 A, 25 L/min, 8 cm/min) exhibited the largest negative error (−0.063 mm), while Run 20 (170 A, 10 cm/min) showed a positive deviation (+0.051 mm) (Table 3). These discrepancies likely stem from localized cooling rate variations and altered convective heat transfer at high gas flow rates, which modify the effective thermal gradient. The CCD design prioritizes central parameter space coverage, leaving edge regimes underrepresented. Incorporating additional axial points or employing physics-informed constraints could further refine model generalization in these regions. Nevertheless, the ANN consistently captures the dominant thermo-mechanical trends governing transverse distortion. Time series plots indicated that ANN predictions tracked experimental values closely in runs involving extreme parameter combinations, aligning with the theoretical advantage of ANN in capturing complex, higher-order nonlinearities that quadratic polynomials may miss.
4. Conclusions
This study successfully develops and validates an ANN model for predicting transverse distortion in 10 mm TIG-welded mild steel plates. The model achieves rapid convergence (5 epochs) and demonstrates strong predictive accuracy (R2 = 0.911, MSE = 9.41 × 10−6, MAE = 0.018 mm) across a systematically designed parameter space. Error analysis confirms unbiased prediction behavior, with deviations predominantly confined to parameter extremes where thermal boundary conditions shift. The proposed framework provides a reliable, computationally efficient alternative to traditional empirical modeling, enabling pre-weld distortion forecasting and reducing experimental trial-and-error.
Future work should expand the dataset to encompass wider plate thicknesses and alloy variants, integrate uncertainty quantification through Bayesian neural networks, and explore real-time deployment for closed-loop process control.