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Purpose

Neighbor interactions among representative volume elements induce systematic perturbations in their effective stiffness and Poisson's ratio when these units are embedded in larger composite structures. However, classic homogenization treats each unit's effective properties as invariant, regardless of the surrounding microstructure. To bridge this gap at minimal cost, we introduce a multi-fidelity homogenization framework augmented by a convolutional neural network correction.

Design/methodology/approach

First, 2D unit cells are homogenized and then assembled into large structures via layout matrices. For each unit, its neighborhood is encoded into a two-channel input and passed to high-capacity neural network models, which predict the local deviations from baseline effective properties. Then, the homogenization results of each unit cell within an assembled structure are corrected correspondingly.

Findings

This approach eliminates more than 92.42% of expensive full-fidelity simulations, yielding a 22-fold speed-up. To enable deployment in resource-constrained or high-throughput settings, we then systematically prune and reorganize the neural network architectures into a lightweight model that trains in under 30 min on a single graphics processing unit and achieves five times faster inference with comparable accuracy (over 80% of the high-fidelity accuracy can be recovered). Convergence and generalization studies confirm that the model remains robust and scalable across unseen configurations, paving the way for rapid structural design and optimization campaigns.

Originality/value

This study introduces a convolutional neural network-enhanced multi-fidelity framework for designing and optimizing fiber-reinforced composite structures intended for segmental failure. Unlike previous works focused on material behavior and fabrication, this research preliminarily addresses the unexplored gap of integrating design, performance prediction, and geometry-driven optimization. The framework enables fast, accurate and scalable exploration of local geometry effects, delivering a damage-tolerant, energy-absorbing composite structure that enhances resilience.

Lightweight fiber-reinforced materials (FRM) have emerged as essential materials in various engineering domains due to their exceptional strength-to-weight ratios and customizable behaviors (Talreja and Waas, 2022; Duan et al., 2025; Dou et al., 2025), including aerospace, automotive, and civil engineering. Their structural composition heavily influences their mechanical performance, particularly the arrangement of fibers and the type of filler materials used within the matrix (Nguyen-Thanh et al., 2022). By integrating multiple representative units, each featuring distinct fiber trajectories and filler compositions, engineers can design advanced composite structures with properties precisely tailored to meet the demands of specific applications (Zhu et al., 2025; Niu et al., 2024; Hyde et al., 2020).

However, identifying the optimal combination and spatial arrangement of these unit cells can become computationally prohibitive as more unit cells are introduced, limiting design innovation and efficiency. To overcome this, various advanced computational optimization techniques have been explored, including evolutionary algorithms (Wang and Sobey, 2020; Cai and Aref, 2015), reinforcement learning (Shen et al., 2025; Li et al., 2024d), Bayesian optimization (Coelho et al., 2025), swarm intelligence methods (Martínez-Muñoz et al., 2023), and neural network-based methods (Li et al., 2024d; Zhan et al., 2025). These approaches can explore the extensive design space within an affordable computational cost by strategically selecting and evaluating promising unit cell configurations. Nevertheless, full simulations on the mechanical behaviors of massive combinations are required for each of these methods (Shih et al., 2023; Barbero and Barbero, 2023). When dealing with large amounts of design variations, these methods show less efficiency. Current advancements on minimizing the number of full simulations while still identifying high-performance designs are neural network (NN) models (Li et al., 2024c; Kim et al., 2023), multi-fidelity simulations (Ahn et al., 2022; Pan et al., 2025), transfer learning from small simulations (Kim et al., 2021; Wang et al., 2025), and active learning coupled with Bayesian optimization (Zhao et al., 2024), etc.

Among these advanced methodologies, the multi-fidelity (MF) simulation method has recently gained considerable attention due to its ability to balance computational efficiency with predictive accuracy (Wang et al., 2024; An et al., 2023; Liu et al., 2024b). Traditional MF simulations run fast, low-fidelity simulations (homogenized unit cells) first to search for high-performance candidates (Li et al., 2024b, 2025). Then, high-fidelity finite element analyses (FEA) will be conducted on these high-performance candidates to identify the optimal combination further. Although homogenized models can save excessive computational resources, they often sacrifice accuracy (interactions between different local units not thoroughly considered), potentially posing threats of error that propagate into optimization outcomes. Moreover, the process of calibrating and validating low-fidelity models against high-fidelity simulations can be computationally expensive and labor-intensive. These considerations are the focus of this paper.

Introducing machine learning into the MF workflow can improve the predictive accuracy. Recent machine learning (ML)-based homogenization methods learn a mapping from micro-structural descriptors to global effective properties of a single representative volume element (RVE), and most MF pipelines use such predictions to screen candidates prior to high-fidelity analyses (Lee et al., 2023). Deep Material Networks approximate RVEs via hierarchical building blocks with guaranteed kinematic/traction compatibility, offering strong accuracy but nontrivial training cost and limited handling of spatial context across interacting units (Su et al., 2022). U-Net-style NN learn pixel-to-property mappings directly from image RVEs (Croom et al., 2022); variants include encoder–decoder NNs for elasticity/thermal fields and attention/U-Net hybrids that improve spatial feature reuse. Graph neural networks (GNNs) (Storm et al., 2024) and message-passing models operate on phase/voxel graphs, capturing long-range dependencies and irregular topologies; extensions include graph U-Nets and spectral GNNs for field prediction. Earlier surrogate-based homogenization combined handcrafted descriptors (e.g. 2-point correlations) with regressors (Bishara et al., 2023). These methods typically return global RVE properties for an isolated cell and do not model unit-level property shifts induced by local neighbors in an assembled structure.

In contrast, this study introduces a novel convolutional neural network (CNN)-based optimization approach into the multi-fidelity simulation framework to improve accuracy and efficiently identify the optimal configurations of RVE, each characterized by unique fiber arrangements and fillers (numerically encoded). CNNs were chosen because the spatial configuration of local RVEs in the composite structure can be naturally represented as two-dimensional matrices, analogous to image data. This makes CNNs particularly effective for capturing RVE interactions and spatial correlations that directly influence the effective material properties. We conducted FEAs separately on RVEs with all phases explicitly modeled to complete homogenization. Spatial arrangements of RVEs were encoded through a series of n × m layout matrices. High fidelity simulations on the RVE assemblies were conducted to identify the property deviations of the same RVE under different surrounding geometries. For each RVE in the assemblies, the local influence is quantified and stored as Pytorch tensors for subsequent training of convolutional neural networks (CNN) (Liu et al., 2024a). The trained models achieve a significant improvement in error compensation and reduction in computational cost without repeated high-fidelity simulation. By systematically removing some layers, a lightweight CNN model that shows comparable ability in capturing the nonlinear local influences with standard CNN models is proposed.

To be more specific, this work contributes: (1) a unit-level, local-neighbor correction that predicts geometry-dependent ratios deviations for each embedded unit cell inside an assembly, rather than only estimating bulk properties of an isolated RVE; (2) a two-channel spatial encoding that preserves both macro-scale layout (cell identifiers) and meso-scale phase content (feature matrices), enabling the CNN to learn short-range interactions; (3) an NN-informed MF selector that applies these corrections to re-rank candidates at low cost, recovering HF quality while promoting a smaller fraction of designs; and (4) a lightweight CNN with block-wise down-sampling that achieves accuracy comparable to deep benchmarks with substantially lower training time and inference latency. We further provide a computational efficiency analysis demonstrating HF savings under identical hardware and solver settings.

The principle of homogenization (Li et al., 2025; Jain, 2019) is replacing the original elements within a specific volume/area with homogenized global material properties, ensuring the homogenized elements store approximately the same amount of strain energy as the original elements. In numerical homogenization, the properties of FRMs are commonly determined by modeling RVEs, which capture the key characteristics of the underlying structure (Jain, 2019).

2.1.1 Generation of representative unit cells

To form the fundamental RVEs, five 2-dimensional, square unit cells with a length of L, each featuring unique internal fiber paths and filler material distributions, were modeled using the Abaqus FEA package as illustrated in Figure 1.

These unit cells serve as the basic components for assembling larger composite structures with tailored mechanical performance. Each unit consists of three different phases: a Polypropylene (PP) matrix (Hossain et al., 2024), which performs as a stable base; Several embedded carbon fibers, which offer strength; and fillers, strategically positioned to boost energy absorption and vibration control (Ramesh et al., 2022). The specific arrangement and interaction of these three phases within each unit cell are critical in determining the overall mechanical performance of the formed structure.

The start and end points of inner fibers are set at every 1/3L points on the edges of each square block to ensure the continuity of fibers in adjacent blocks when assembled. The PP matrix was treated as an isotropic elastic-plastic material defined by its Young's modulus and Poisson's ratio. Plasticity of PP was specified in Abaqus via a table of yield stress and plastic strain pairs (no kinematic hardening or rate dependence was included). Fillers were treated as a linear elastic material. For the carbon fibers, an orthotropic elastic model was used, implemented in Abaqus via engineering constants. Detailed material properties are listed in Table 1.

Mesh convergence was first established at the RVE level by refining matrix/filler and fiber seeds until changes in E11, E22, ν12 were less than 1%. Specifically, three refinement levels were considered: (1) Matrix/filler seed 0.0060 mm, fiber seed 0.0020 mm. (2) Matrix/filler seed 0.0045 mm, fiber seed 0.0015 mm. (3) Matrix/filler seed 0.0030 mm, fiber seed 0.0010 mm.

For each unit cell, the effective stiffness and Poisson's ratio were computed at each refinement level under the same macroscopic loading. Across all cases, differences between level 2 and level 3 satisfied the precision criteria (less than 1%). Eventually, the meshing seed size of the PP matrix was set as 0.0045 mm, while the carbon fibers, which experience higher stress gradients and require higher accuracy, are refined to a seed size of 0.0015 mm.

2.1.2 Implementation of periodic boundary conditions and macroscopic strain

Applying periodic boundary conditions (Tian and Qi, 2023) (PBC) to each unit cell is critical to accurately simulate the unit cells' mechanical response and ensure continuity across adjacent units. This approach allows the models to mimic infinite composite material by ensuring that the displacements and tractions on opposing boundaries remain consistent, thereby preserving the representativeness of the micro mechanics in larger-scale assemblies. Figure 2 shows the principle of PBC application on the boundaries of each unit cell.

To apply the PBCs rigorously, we begin with the deformation gradient tensor F:

(1)

where I is the identity tensor and ▽u is the displacement gradient tensor. The general periodicity condition for a unit cell of length L in each direction is:

(2)

where ɛ is the sympmetric macroscopic strain tensor under small deformation assumptions. Expressed in component form for square unit cells:

(3)
(4)
(5)
(6)

These relations enforce a displacement field that is periodic while allowing a uniform average strain to develop across the RVE.

Following the implementation of PBCs, multiple reference points (RP) were introduced and kinematically coupled to the boundary nodes of the unit cells with the multi-point constraints (MPC) method (Tian and Qi, 2023). The periodic constraints were implemented in Abaqus using the *EQUATION command. Nodes on opposite boundaries were paired according to their coordinates, and their displacements were coupled through linear constraint equations (Wang et al., 2025; Qi et al., 2015). The macroscopic strain components were represented by reference points (RPs) whose prescribed displacements correspond to ɛ11Lx, ɛ22Ly, and ɛ12Lx, ɛ12Ly. For example, the constraint between the left and right boundaries was defined as.

  • *EQUATION

  • 3, Rnode,1,1.0, Lnode,1,-1.0, RP_EXX,1,-1.0

  • *EQUATION

  • 3, Rnode,2,1.0, Lnode,2,-1.0, RP_GXYx,1,-1.0

Analogous equations were applied for the top and bottom boundaries.

2.1.3 Homogenized properties

For each unit cell, three independent loading conditions were applied: uniaxial tension in the x and y direction, and shear in the x-y plane. The effective stiffness components were calculated using the volume-averaged form of Hooke's law (Jain, 2019):

(7)

Where σ¯ij is the average stress tensor components over the unit, ε¯kl is the applied average strain tensor components, Eijkleff is the effective stiffness tensor of the unit cell. For 2D plane stress or plane strain, the fourth-order stiffness tensor (Bauer and Böhlke, 2022) reduces to a symmetric 3 × 3 matrix using Voigt notation:

(8)

where E11 and E22 are the effective axial stiffness in x and y direction, E12 is the coupling between ɛ11 and σ22, E66 is in-plane shear modulus. These were computed by solving the system of equations generated from the three loading cases. The macroscopic stress σ¯ij can be calculated by volume/area averaging:

(9)

This integration is implemented in Abaqus using field output averaging over the entire unit cell area. Through defining ɛ11 ≠ 0, ɛ22 = ɛ12 = 0, E11 and E12 can be extracted. Similarly, E22 and E12 can be extracted through defining ɛ22 ≠ 0, ɛ11 = ɛ12 = 0. The corresponding effective properties were derived as:

(10)
(11)
(12)

All simulations were run in Abaqus (standard) under a 2-D plane-stress assumption with nominal thickness 1.0 mm and all models were built using CPS4R elements with reduced integration and hourglass control enabled. Frictionless contact was assumed for the elastic simulations, while continuity across unit boundaries and interfaces was enforced using tie constraints.

From the resulting stiffness tensors, the effective Young's modulus E and Poisson's ratios ν were extracted for each unit cell. These homogenized properties were later used as key parameters to construct representative, low-fidelity models and served as baseline properties (denoted as Eeff and νeff) for comparison in the multi-fidelity framework.

2.2.1 Assembly rules

Before assembly, the unit cells were encoded using a unique integer identifier ranging from 1 to 5. Through randomly positioning the integers into a series of two-dimensional arrangement matrices of size n × m, diverse spatial configurations of the larger composite structures with size nL × mL were generated. The arrangement matrices serve as a spatial encoding of specific composite structures, where the position of each integer reflects the placement of a particular unit cell within the global structure (Figure 3). Such encoding methods allow for efficient and scalable input generation for both high-fidelity simulations and NN models. Each matrix encodes not only the constituent types but also the geometry information of unit cells, which is essential for capturing local-neighbor influences.

After translating the unit cells into the grid, dedicated node sets were created for every unit. These node sets include all relevant phases within each unit and serve as spatial references for post-processing the stress and strain fields at the unit-cell level using Python scripts. Figure 4 shows a representative of the composite structures built with 30 randomly generated 20 × 20 arrangement matrices. Only simulation results of structures 1 to 25 were collected for NN training.

Unlike the typical homogenization process that extracts bulk properties of the entire structure (Li et al., 2024c), the focus here is on the local homogenized properties of individual unit cells within the structure. The effective properties of a specific unit vary not only depending on its composition but also on the geometrical arrangements of its neighboring units (Ramesh et al., 2022; De et al., 2024). For instance, unit 1 may exhibit different effective behavior when surrounded by different geometrically distributed unit cells, as shown in Figure 5.

By comparing these context-sensitive effective properties against the baseline properties obtained from single-unit-cell simulations, the influence of spatial interaction can be quantified.

2.2.2 Simulation on the assembled structures

Parallel simulations were conducted on the assembled structures. The ground truth responses of the structures were captured through high-fidelity simulation, where the fibers, fillers, and matrix phases within the assembled structures remain explicitly resolved (Cheung and Mirkhalaf, 2024; Li et al., 2024a). Meanwhile, the homogenized surrogate behaviors of the structures were captured through standard low-fidelity simulation, where the three phases within the units were replaced with equivalent properties.

Global loading conditions were applied using the same RP-driven approach to simulate the mechanical behavior of the structures. Specifically, PBC was applied to ensure continuity and compatibility with the behavior of the unit cells, thereby capturing the effective macroscopic response. To ensure mechanical continuity throughout the structure, the adjacent boundaries of units are connected through tie constraints. Similarly, fibers were also tied across unit boundaries to preserve the intended load transfer pathways and maintain microstructural realism.

Prescribed vertical displacements corresponding to a 1% global strain in the y direction were then applied to the RPs, inducing a uniform tensile load across the height of the structure. This setup ensures consistent global deformation, enabling stress responses to be computed across all embedded units.

2.2.3 Local geometry influences observation

The homogenized properties of each unit cell within its local environment were calculated through the volume-averaging method. This enabled a direct comparison between the baseline effective property Eeff(obtained from isolated simulation) and the local-neighbor-influenced effective property Eln,eff when the same unit cell is embedded in different spatial geometries.

To quantify the effect, Eeff to Eln,eff ratio Re and νeff to νln,eff ratio Rν were introduced. We analyzed the Re and Rν of all unit cells across a series of geometrical configurations. Figure 6 illustrates the Re and Rν scatter plots of each unit cell across 30 randomly selected geometries extracted from the 25 structures.

The results reveal that the stiffness component (particularly in the loading direction) exhibits the most significant variation, suggesting that the load transfer paths and constraint effects attributed to neighboring units play critical roles in modulating local behavior (Liu et al., 2022; Bauer and Böhlke, 2022). This observation supports the need to incorporate local-neighbor effects into the modeling framework. The use of an NN model to capture these nonlinear interactions becomes essential for boosting the predictive accuracy of low-fidelity models without incurring the computational cost of full high-fidelity evaluations.

2.3.1 Encoding method

For each arrangement matrix, a series of 5 × 5 submatrices was extracted to represent the local geometry surrounding a target unit cell, as illustrated in Figure 7. The center of a submatrix corresponds to the target unit x, whose homogenized property variations under local-neighbor interaction are to be predicted. The first surrounding layer, which directly contacts unit cell x, is assumed to impose local influence on unit x's mechanical behavior. The second surrounding layer is considered to introduce neighboring influences, affecting how stress is transferred and distributed through the structure.

By systematically sliding this window across an arrangement matrix (padding the edge units that lack a full neighborhood with zeros), a set of local geometry sub-matrices can be extracted from a single assembled structure. Specifically, from each n × m arrangement matrix, up to nm valid sub-matrices of size 5 × 5 can be generated (duplicated sub-matrices were removed). Each extracted 5 × 5 sub-matrix is then transformed into a two-channel 500 × 500 input array for the CNN. For the first channel, each integer in the 5 × 5 matrix, representing unit cell types and padding, is expanded into a corresponding 100 × 100 block using nearest-neighbor upsampling. This creates a 500 × 500 matrix preserving the original spatial arrangement at an enhanced resolution suitable for CNN processing.

The second channel encodes internal structural information of each unit cell type through predefined feature matrices. Six 100 × 100 feature matrices (including the value 0 in the padding area) were generated based on finite-element analysis images of the internal microstructure, representing the spatial distribution of matrix, fiber, and filler phases, and numerically encoded with distinct mechanical property values. Initially, the internal phase information of each unit cell was identified by segmenting RGB images obtained from FE simulations. As shown in Figure 8, each color region corresponded uniquely to one of the internal phases (matrix, fiber, or filler). Subsequently, these RGB-segmented images were translated into numerical feature values representing the distinct mechanical properties assigned to each phase.

The resulting numerical arrays form feature matrices that explicitly encode the heterogeneous internal composition of each unit cell. Each element in the original 5 × 5 arrangement matrix is then mapped to its corresponding feature matrix according to the unit type number. The mapped 100 × 100 feature matrices are subsequently assembled into a second 500 × 500 matrix, spatially matching the first channel. Each two-channel input effectively captures both the macro-scale geometric configuration and the meso-scale physical composition, enabling the neural network to learn local neighbor influences accurately.

2.3.2 Dataset generation

After assembling all two-channel 500 × 500 input arrays, the complete dataset was compiled into a single NumPy file for efficient loading and access during model training. Each input sample in this dataset corresponds to a unique local neighborhood configuration extracted from a larger composite structure, paired with its respective target output values Re and Rν. The generated input dataset has a shape of (N, 2, 500, 500), where N denotes the total number of samples (N = 10,000 in this study), 2 represents the two input channels, and 500 × 500 corresponds to the spatial resolution of each sample derived from assembling 5 × 5 unit cells, each mapped to a 100 × 100 feature region.

Based on previous observations, the stiffness component aligned with the primary loading direction exhibits the greatest sensitivity to local-neighbor influences (Ramesh et al., 2022; Wang et al., 2025). Therefore, only the stiffness component E22 and Poisson's ratio ν21 are considered for inclusion in the output vector during dataset preparation. For each of the 5 × 5 sub-matrices, the corresponding output vector is calculated as:

(13)

where:

(14)

Considering the models were loaded in y direction, each output sample is a 2-dimensional vector:

(15)

When generated for an entire n × m structure, these outputs form a 3D tensor of shape:

(16)

The output tensors are spatially aligned with the corresponding position matrix of the assembled structure, ensuring a direct mapping between the encoded geometry (input) and the predicted property variations (output). To facilitate neural network training, all input–output pairs are consolidated into structured datasets: each assembly is assigned to exactly one of the sets (train, validation, test), and no structure contributes patches to more than one split. The assignment is implemented with a group-aware splitter keyed by the structure ID (Novac et al., 2022). The input/output datasets were then stored as Pytorch tensors and then split into three parts randomly according to the assignment. 70% of the data sets are used as training sets, 15% for validation, and 15% for evaluation.

Data normalization (Fan et al., 2023) is crucial for achieving stable and efficient training of convolutional neural networks, particularly when input channels exhibit drastically different numerical ranges. Without appropriate normalization, gradient-based optimization methods may struggle to converge, due to numerical instability and uneven scaling between input channels.

In this study, the input data consists of two channels with distinctly different numerical characteristics. The first channel, representing the unit cell type (integers ranging from 0 to 5), was normalized using simple min–max scaling:

(17)

where x represents the original integer value, ensuring the channel's numerical range is constrained within [0, 1].

The second channel, containing the feature matrices with values of 30 (filler), 1700 (matrix), and 135,000 (fiber), exhibited significant numerical disparities. To address this, a logarithmic transformation followed by min–max scaling was applied to compress and standardize the data:

(18)

This normalization technique significantly reduced numerical variance, placing all values within a stable numerical interval of [0, 1]. The effectiveness of the normalization was confirmed by examining the resulting data ranges (Table 2), verifying that both input channels were now suitably scaled for efficient network training.

In addition to input normalization, min–max scaling was also applied to the output dataset, specifically targeting the effective property ratios Re and Rν. The normalization for output data followed a similar linear rescaling:

(19)

where y denotes each property difference or ratio in the original dataset. This step ensured that the network outputs also fall within a bounded range of [0, 1], significantly improving the stability and efficiency of gradient computations during network training.

Data loading was conducted with no parallel workers to maintain reproducibility and stability across platforms. Empirical results demonstrated significantly improved convergence speeds and predictive performance following normalization, underscoring its importance in the neural network training pipeline. After normalization, both inputs and outputs exhibited consistent numerical ranges, leading to enhanced training stability and predictive robustness.

In this study, we selected CNN for predicting Re and Rν due to their inherent capability to efficiently capture and leverage spatial dependencies and local geometric patterns embedded within image-based input data. Unlike fully connected or recurrent neural networks (Sathish et al., 2023; Ghane et al., 2024), CNNs excel at extracting hierarchical spatial features through convolutional kernels, which makes them particularly suitable for processing structured two-dimensional input arrays representing macro-scale geometry and meso-scale internal features of composite materials (Li et al., 2023; Novac et al., 2022). However, standard CNN typically requires extensive computational resources, substantial training durations, and large memory capacities to process high-resolution input data (Li et al., 2024c). These constraints can limit their practical utility, especially when rapid inference or resource-constrained deployment environments are required. Hence, a lightweight CNN architecture employing specialized strategies, such as block-wise down-sampling, was developed. The lightweight model significantly reduces computational complexity and memory footprint while maintaining comparable prediction accuracy to conventional CNNs.

3.2.1 Standard CNN models

We implemented two widely adopted, high-capacity CNN architectures as benchmarks: a baseline CNN model (model-1) and a ResNet-18 network(model-2). Each network was modified (first layer and output layer) to processes the full 2 × 500 × 500 input tensor through its respective stack of convolutional, pooling (or residual) layers and final fully-connected layers to predict the values of Re and Rν. Model-1 (approximately 11M parameters) uses cascades of 3 × 3 convolutions interleaved with max-pooling to compress spatial resolution, whereas Model-2 (randomly initialized, approximately 12.5 M parameters) employs eight residual blocks to ensure stable gradient propagation in a moderately deep topology (Azad et al., 2025). Specific architectures and tunable hyper-parameters for these two baseline models are summarized in Table 3.

The models were trained for 100 and 110 epochs on identical data-augmentation pipelines and optimizer settings. We systematically recorded key performance metrics—training duration, memory footprint, inference speed, and predictive accuracy to establish a rigorous baseline against which we compare our lightweight CNN variants.

3.2.2 Lightweight model

The lightweight CNN model was developed by systematically reducing the complexity of model-1 and model-2, as shown in Figure 9. Unlike the standard models, this lightweight model utilizes a block-wise down-sampling strategy, compressing spatial dimensions into a manageable feature representation without sacrificing the critical spatial and structural information required for accurate prediction. Specifically, given the large input size (N, 2, 500, 500), the input is partitioned into smaller, non-overlapping blocks (block pooling layer). In this context, the CNN employs a convolutional layer with a kernel size and stride equal to the block size (100 × 100). Each block is processed individually by this convolutional kernel, effectively summarizing and compressing localized spatial and structural information into a smaller, lower-resolution feature map (in this case, from 500 × 500 down to 5 × 5). This block-wise pooling mechanism slashes both FLOPs and peak memory usage. Moreover, the entire model comprises approximately 3 million trainable parameters, roughly one-quarter of model-1, enabling training times on the order of 20–30 min and inference latencies below 5 ms per sample, all while matching the predictive accuracy of the larger architectures. This down-sampling strategy significantly reduces computational complexity and memory requirements, while retaining essential spatial patterns and features critical for accurately predicting local effective property ratios.

The block pooling layer transforms the input of size (N, 2, 500, 500) into a representation, where 256 learnable filters extract abstract local spatial features across the downsampled grid. The number of filters in this block-pool layer was increased from the baseline to 256 to improve feature richness and capacity. The output from the block-wise layer is processed through a sequential stack of six convolutional layers with decreasing filter widths. Each convolution uses a kernel size of 3 × 3 with padding of 1, followed by batch normalization and ReLU activation (Song et al., 2023) to promote gradient stability and non-linearity. This deep stack enhances local pattern recognition and supports robust spatially distributed structural effects learning. Following convolutional processing, the 5 × 5 × 8 output is flattened and passed through a FC (Li et al., 2023) head consisting of three hidden layers with dimensions [512, 256, 64], each followed by ReLU activation and dropout (0.4) to reduce overfitting. The final FC layer maps the learned features to the two output targets, representing the normalized Re and Rν values, respectively. All parameters used in the training process of the lightweight model are listed in Table 4.

The CNN models are set up using the Pytorch framework (Novac et al., 2022) according to the above architectures and then trained with the Adam Optimizer (Li et al., 2023; Song et al., 2023; Ghane et al., 2024; Li et al., 2024c). Given the dataset size, the architecture is compact, and an early stopping criterion (Yang et al., 2019) based on validation loss is implemented to minimize the risk of overfitting while still maintaining enough expressive ability to mimic local interactions. At each epoch, training and validation losses, along with scores, were computed and visualized in real-time to monitor convergence behavior. The best model was selected based on validation performance and further evaluated on a held-out test set. All experiments were run on CUDA-enabled GPUs (Nvidia GeForce RTX 3070).

Figure 10 depicts the training and validation loss curves that reflect the training stability by indicating the convergence behavior of both training and validation losses. In the early stage, the training and validation losses of all models both decrease rapidly, indicating stable and effective model learning (Li et al., 2023). As the training epoch grows, the improvement rate (dropping velocity of the loss curves) gradually slows down. The validation losses of model 1 and model 2 plateau after approximately 90th and 70th epoch, respectively, while the training loss continues to decline slightly. Such divergence marks the point where the model begins overfitting. The training processes are halted at 90th and 70th epochs, respectively, to preserve the best generalization performance according to the preset early-stopping criterion (Yang et al., 2019). The stable gap between the training and validation loss curves, along with their smooth convergence behavior, indicates that the CNN models have achieved a good balance between underfitting and overfitting.

For the lightweight model, the dropping rate of its training loss slows down after the 85th epoch. Although it continues to decline modestly through to the 120th epoch, the rate of improvement falls below 0.1% per epoch, indicating diminishing returns. Meanwhile, validation loss reaches its minimum around the 90th epoch, after which it remains effectively flat, suggesting the network has captured the dominant feature mappings. Consequently, we adopt an early-stopping criterion at epoch 100, when validation improvement drops below our 0.05% threshold to prevent overfitting and minimize total training time to under 30 min. This strategy yields a final lightweight model whose test-set RMSE matches the standard models within 2%, while inference latency is reduced by more than 95%.

Figure 11 presents a set of overlaid scatter plots, each comparing the CNN-predicted values of the normalized effective stiffness ratio Re (left panel) and the normalized Poisson's ratio Rν (right panel) against the corresponding ground-truth data from the validation set. Points are color-coded by model type (model-1, model-2, and lightweight Model), with the solid black line denoting the ideal y = x relationship.

On both axes, values span the interval [0.83, 1.18], capturing the full range of local property perturbations induced by varying 5 × 5 neighborhoods (Hyde et al., 2020). All three models produce a tight cluster of points around the identity line, with negligible systematic bias or spread even in regions of extreme neighbor effects. Model-1 and Model-2 achieve root-mean-square errors of approximately 0.015, while the lightweight Model, despite its drastically reduced parameter count, attains an RMSE of just 0.017 for Re and 0.013 for Rν.

This visualization confirms that each network, and in particular our optimized lightweight architecture, robustly approximates the nonlinear mapping from local geometry to effective property corrections. The near-perfect alignment with y = x further demonstrates the models’ capacity to generalize across hundreds of assembly configurations, enabling rapid, high-fidelity microstructure predictions without resorting to costly full-scale finite-element simulations (Cheung and Mirkhalaf, 2024; Li et al., 2024a).

The homogenization quality of unit cells 1–5 was further validated by direct comparison with full-fidelity FE models of the same microstructures. Figure 12 displays the equivalent uniaxial stress–strain responses for each homogenized unit cell overlaid with the corresponding high-resolution simulation results. In every case, the two curves exhibit closely initial slopes (effective Young's moduli) and yield points, with maximum deviations below 5% in stress.

These comparisons confirm that our homogenized constitutive models faithfully reproduce the key mechanical behaviors—linear stiffness, onset of nonlinearity, and post-yield softening of the detailed micro-structural simulations (Wen et al., 2024; Barbero and Barbero, 2023). Such close alignment not only validates the baseline effective properties but also demonstrates that the reduced, homogenized representation captures the essential physics needed for accurate downstream predictions in both the standard and lightweight CNN frameworks.

Traditional homogenization treats each unit cell as possessing a fixed, context-independent set of effective properties, thereby overlooking the perturbations introduced by the neighboring environment (Li et al., 2024c). In contrast, our CNN-augmented frameworks explicitly account for these local interactions and predict the resulting property discrepancies. To evaluate its accuracy, we compare three sets of predictions: standard homogenization, NN corrections, and full-fidelity simulation results, using the deviation metrics as follows:

(20)
(21)

where E22full and ν21full stand for ground truth value of E22 and ν21 respectively. Similarly, the prediction errors of NN model can be expressed as:

(22)
(23)

where δNN and γNN are errors of NN predicted effective stiffness and Poisson's ratio, respectively. For a cell within its local geometry, a higher value of δhom reflects strong neighbor influence, whereas a lower value of δNN indicates the NN correction effectively compensates for the deviations. Conversely, a smaller δhom implies negligible neighbor influences.

Based on the quantified errors, two indicators, Ie and Iν, are introduced to assess both the extent of deviations of homogenized properties from the ground truth value and the accuracy of NN correction within a cell's local geometrical context, as follows:

(24)
(25)

A higher value of I indicates higher homogenization error and greater error reduction through NN correction. In Figure 13, the heatmap shows the improvement ratios I of the three CNN models across unseen structure (specifically, structure No.27). The color gradations in the heatmap indicate how good the NN correction works. Regions with darker colors reflect lower improvements (lower values of I), while lighter areas indicate larger improvements.

Across all three models, a large majority of locations recover at least 80% of the high-fidelity correction. Furthermore, the models exhibit similar patterns, with the highest improvement ratios generally observed in regions where local influences are more pronounced. Indeed, the intrinsic error of the homogenization can substantially bias the initial candidate ranking. The designs with target performance that barely clear the threshold may be underestimated and discarded, creating false negatives. This spatial analysis supports the assertion that the incorporation of local geometry information significantly boosts prediction performance.

Furthermore, three simulation strategies were implemented on the unseen Structures: full-fidelity simulation, homogenized simulation, and homogenized simulation with NN corrections, enabling a rigorous assessment of the models' ability to extrapolate beyond known data. Results show that the model exhibited stable performance when predicting Re and Rν for unit cells embedded in unfamiliar environments.

The comparison between the full fidelity simulation and the homogenized simulation informed by the lightweight NN model, as shown in Figure 14, reveals the effectiveness of homogenization in simplifying complex composite behavior (Bauer and Böhlke, 2022). In the full model (left), stress and strain distributions show significant local variations due to fiber-matrix interactions and geometric complexities, reflecting microscale heterogeneity. In contrast, the homogenized model (right) exhibits smoother, more uniform fields, indicating that local effects have been averaged into effective material properties. The lightweight model informed result (center), however, exhibits a much closer match to the full-fidelity result. Notably, the red dashed circle highlights regions where the NN-informed model successfully recovers stress intensification patterns absent in the conventional homogenized model, thereby demonstrating its ability to reconstruct local stress effects without explicitly modeling the fine-scale geometry. The strain field shows similar trends. The lightweight model informed simulation captures both magnitude and spatial variation better than the standard model, which oversimplifies deformation. Overall, the lightweight CNN effectively reconstructs local effects, offering high-fidelity mechanical response with reduced computational cost, validating the proposed multi-fidelity framework.

Figure 15 depicts the equivalent stress–strain curves obtained from the simulation results. The standard homogenized model significantly underestimates the stress response, particularly beyond the elastic regime, due to its inability to account for local stiffness variations and stress intensification. In contrast, the CNN-informed and lightweight models provide stress–strain predictions that closely track the full-fidelity curve across the entire deformation range.

Importantly, despite a dramatic reduction in parameters and compute, the lightweight model maintains accuracy on par with the standard CNN models. By systematically pruning convolutional layers and adopting a block-wise, down-sampling strategy, the lightweight model achieves comparable R2 and error statistics (within 5% of the standard model), while reducing training time to under 30 min and inference latency by over 10-fold. Such a level of predictive accuracy and robustness supports the model's suitability for accelerating exploration of targeted composite design without the computational burden of full-scale simulations (Cheung and Mirkhalaf, 2024).

An essential motivation for integrating NN corrections into the multi-fidelity framework is to reduce the overall computational cost with enhanced accuracy (Ghane et al., 2024). To quantify the NN models' efficiency, we compared three strategies on a representative set of 500 combinations using the three CNN models.

  1. Full fidelity (FF) simulation for baseline: Structures are simulated by high fidelity FEA.

  2. Standard multi-fidelity simulation (MF): all 500 structures undergo fast, low-fidelity homogenization; the top 10% by low-fidelity ranking are then re-evaluated with high-fidelity FEA.

  3. NN informed multi-fidelity (NN-MF): as in the MF approach, but the NN correction is used to adjust low fidelity estimates and re-rank candidates. Only the top 4% are promoted to high fidelity FEA (NN-MF at 4% matched the top objectives achieved by MF at 10%).

All methods were applied to the same 500 assembled combinations, generated once with a fixed random seed. No candidates were added or removed between methods. MF ranks by the baseline homogenized objective; NN-MF ranks by the same objective after applying the CNN ratios to the effective properties. If multiple designs tie at the boundary score, selection is made deterministically by: (1) secondary key equals lower predicted variance, then (2) lexicographic index of the layout (row-major). No FF warm starts were used (to avoid bias). Geometry assembly, node or face sets, and meshing templates were cached and reused across methods; solver tolerances, element types, and hardware settings were identical for MF and NN-MF to ensure fair wall-clock comparisons. All running times were recorded on a 12-core AMD Ryzen9 5900X (3.7 GHz, 32 GB RAM) for CPU-bound homogenizations, and a single NVIDIA RTX 3070 GPU (8 GB) for NN inference. Detailed computational costs on training and inference per structure are listed in Table 5.

Table 6 shows the comparison of computational time cost for the 500 configurations. The standard MF strategy already cuts the simulation time by nearly 90% compared to FF evaluation. Incorporating the NN correction further halves this cost, yielding a total speed-up of over 22-fold relative to the baseline FF strategy, with negligible overhead of NN inference for all 500 samples.

The cost of low-fidelity simulation scales linearly with the number of candidates and remains small per sample (Cheung and Mirkhalaf, 2024); full-fidelity analyses are surely the dominant term in the entire optimization workflow. By dynamically adjusting that term with NN-based re-ranking, the NN-informed multi-fidelity workflow scales very favorably: doubling the design space induces only a proportional increase in low-fidelity cost and NN inference, while the number of full-fidelity simulations can be held roughly constant to maintain a given accuracy level. These results demonstrate that our Lightweight CNN strikes an optimal balance, maintaining parity in accuracy with deeper benchmarks while drastically reducing computational cost and resource demands.

This work has introduced and validated a neighbor-aware, NN correction within a multi-fidelity homogenization framework to predict effective property deviations of composite structures assembled from 2-dimensional RVE unit cells. The main findings include.

  1. Local-neighbor influence captured by NN model. By encoding each unit's local context into a 5 × 5 matrix and training the NN model to predict the deviation, over 80% of the high-fidelity accuracy can be recovered while only requiring a small portion of full FE solves.

  2. Models’ generalization to unseen assemblies. When evaluated on previously unseen structures, the NN predictions maintain sub-10% error on effective property deviations.

  3. Substantial Computational Savings. By systematically pruning the architecture of conventional CNN models and implementing a down-sampling strategy, our lightweight model achieves a 92.42% reduction in total simulation cost while holding error below 10%.

Despite these promising outcomes, the approach has clear limitations. The training dataset is obtained from FEA on planar 2-dimensional unit cells with minor plastic behavior (Xu and An, 2022); extensions to 3-dimensional units or to inelastic and damage-evolution models would require retraining on higher-dimensional data (multi-channel inputs) and potentially more complex NN architectures. Likewise, while a fixed 5 × 5 local window proved sufficient for the materials and layouts studied here, highly anisotropic fiber trajectories or graded-volume architectures may demand adaptive neighborhood sizes or trainable attention weights. Given the localized, normalized targets and strong cross-structure heterogeneity, single scalars may obscure systematic, context-dependent effects. Accuracy is instead summarized via by-structure splits and steady-state validation R2, future work may add complementary error metrics. Finally, the model has so far been demonstrated on a regular three-phase system (Tian and Qi, 2023; Cheung and Mirkhalaf, 2024); material systems with vastly different phase contrasts or interface behaviors will require further transfer-learning experiments to verify data efficiency and accuracy.

Future developments will extend the framework to include full plasticity and damage evolution to capture nonlinear and dissipative behaviors of composites. The approach will also be scaled to larger assemblies to examine size convergence of effective properties. Methodologically, adaptive neighborhood learning using attention or graph-based models, uncertainty-guided active sampling, and physics-informed loss functions enforcing mechanical symmetry and bounded corrections will be explored to enhance robustness and extrapolation to highly heterogeneous configurations (Ghane et al., 2024). Additionally, the methodology will be extended to three-dimensional simulations to capture out-of-plane interactions and validate its robustness for realistic composite architectures.

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Published by Emerald Publishing Limited. This article is published under the Creative Commons Attribution (CC BY 4.0) license. Anyone may reproduce, distribute, translate and create derivative works of this article (for both commercial and non-commercial purposes), subject to full attribution to the original publication and authors. The full terms of this license may be seen at Link to the terms of the CC BY 4.0 licence.

Data & Figures

Figure 1
A diagram shows five square composite material units labeled “Unit‑1” to “Unit‑5”.The diagram displays five separate square tiles representing composite material microstructures. Each tile contains a blue background region labeled “Matrix”, curved beige bands labeled “Fiber”, and circular light gray inclusions labeled “Filler”. “Unit‑1” appears in the top left and includes two semicircular, one curved, and one diagonal fiber path and two circular fillers. “Unit‑2” appears in the top center and shows two main diagonal and two semicircular fibers crossing the tile with two circular fillers near opposite corners. “Unit‑3” appears in the top right and contains large curved fiber arcs near the top-right and bottom edges, with two circular fillers on the left. “Unit‑4” appears at the bottom left and shows a central vertical fiber connected to two large curved fibers forming a U shape, with two circular fillers near the upper corners. “Unit‑5” appears at the bottom right and displays multiple intersecting curved fibers creating a network across the tile, with three circular fillers placed near the top left, center, and bottom right.

Overview of all five 2D unit-cell geometries with distinct fiber paths and filler layouts, and corresponding finite-element meshes, showing element sizing (matrix: 0.0045 mm, fiber: 0.0015 mm)

Figure 1
A diagram shows five square composite material units labeled “Unit‑1” to “Unit‑5”.The diagram displays five separate square tiles representing composite material microstructures. Each tile contains a blue background region labeled “Matrix”, curved beige bands labeled “Fiber”, and circular light gray inclusions labeled “Filler”. “Unit‑1” appears in the top left and includes two semicircular, one curved, and one diagonal fiber path and two circular fillers. “Unit‑2” appears in the top center and shows two main diagonal and two semicircular fibers crossing the tile with two circular fillers near opposite corners. “Unit‑3” appears in the top right and contains large curved fiber arcs near the top-right and bottom edges, with two circular fillers on the left. “Unit‑4” appears at the bottom left and shows a central vertical fiber connected to two large curved fibers forming a U shape, with two circular fillers near the upper corners. “Unit‑5” appears at the bottom right and displays multiple intersecting curved fibers creating a network across the tile, with three circular fillers placed near the top left, center, and bottom right.

Overview of all five 2D unit-cell geometries with distinct fiber paths and filler layouts, and corresponding finite-element meshes, showing element sizing (matrix: 0.0045 mm, fiber: 0.0015 mm)

Close modal
Figure 2
A diagram shows a finite element model of a red square composite plate with mesh and labels.The diagram depicts a finite element mesh of a square composite plate in the x-y plane, with a red-shaded domain bounded by length L. The mesh consists of the quadrilateral elements forming curved U-shaped bands within the red matrix, with two blue circular regions at the upper left and right regions. Four circular nodes labeled M subscript i on the left, M subscript k at the top left, M subscript j at the right, and M subscript l at the bottom left represent embedded components or cutouts at the edges. The triangular fixed supports labeled N subscript 1, N subscript 2, and N subscript 4 are shown at the bottom left, bottom right, and top left corners, respectively. A circular node labeled N subscript 3 is shown at the top right corner. A strain coordinate system labeled “R P 1” with “epsilon subscript 21” extending right and “epsilon subscript 22” extending upward is shown above the top edge of the plate. Another strain coordinate system labeled “R P 2” with “epsilon subscript 11” extending right and “epsilon subscript 12” extending upward is shown on the right of the plate. At the bottom right, a coordinate system shows origin O, the horizontal x-axis, and the vertical y-axis.

Periodic boundary conditions on unit cells

Figure 2
A diagram shows a finite element model of a red square composite plate with mesh and labels.The diagram depicts a finite element mesh of a square composite plate in the x-y plane, with a red-shaded domain bounded by length L. The mesh consists of the quadrilateral elements forming curved U-shaped bands within the red matrix, with two blue circular regions at the upper left and right regions. Four circular nodes labeled M subscript i on the left, M subscript k at the top left, M subscript j at the right, and M subscript l at the bottom left represent embedded components or cutouts at the edges. The triangular fixed supports labeled N subscript 1, N subscript 2, and N subscript 4 are shown at the bottom left, bottom right, and top left corners, respectively. A circular node labeled N subscript 3 is shown at the top right corner. A strain coordinate system labeled “R P 1” with “epsilon subscript 21” extending right and “epsilon subscript 22” extending upward is shown above the top edge of the plate. Another strain coordinate system labeled “R P 2” with “epsilon subscript 11” extending right and “epsilon subscript 12” extending upward is shown on the right of the plate. At the bottom right, a coordinate system shows origin O, the horizontal x-axis, and the vertical y-axis.

Periodic boundary conditions on unit cells

Close modal
Figure 3
A schematic diagram shows patterned units mapped into an arrangement matrix and assembled into a larger grid.On the left, five square patterned tiles are shown with distinct fiber paths and circular fillers. “Unit‑1” appears in the top left and includes two semicircular, one curved, and one diagonal fiber path and two circular fillers. “Unit‑2” appears on the middle left and shows two main diagonal and two semicircular fibers crossing the tile with two circular fillers near opposite corners. “Unit‑3” appears at the bottom left and contains large curved fiber arcs near the top-right and bottom edges, with two circular fillers on the left. “Unit‑4” appears at the center and shows a central vertical fiber connected to two large curved fibers forming a U shape, with two circular fillers near the upper corners. “Unit‑5” appears below unit-4 and displays multiple intersecting curved fibers creating a network across the tile, with three circular fillers placed near the top left, center, and bottom right. Rightward arrows with numbers “1”, “2”, “3”, “4”, and “5” from these units indicate how these units are referenced. At the center is a rectangular numerical table labeled “Arrangement matrix n by m” below the grid. The matrix consists of ten rows and ten columns. Each cell contains a single integer value between 1 and 5. The numbers are evenly spaced and aligned, forming a clear grid without visible row or column headers. In the top-left corner of the matrix, the first row begins with the sequence “1, 3, 1, 5”, and the second row begins with “3, 2, 5, 4”. These initial cells are lightly shaded in different colors, visually distinguishing them from the rest of the table. The remaining cells are unshaded and contain only numeric characters on a white background. These numbers correspond to the unit labels shown on the left. Curved arrows above the matrix point from selected numbers in the matrix toward the right side of the figure. On the right, a larger grid labeled “Assembly n dot L times m dot L” shows an expanded layout. The grid is divided into ten evenly spaced rows and ten columns with visible cell borders. In the upper-left portion, several rows contain numeric values from 1 to 5 arranged in a structured pattern. In the first row, the cells contain “1, 3, 1, 5, 2, 4, 3, 5, 1, 2”, and in the second row, the cells contain “3, 2, 5, 4, 1, 2, 4, 3, 5, asterisk”, with the numeric cells lightly shaded in different colors, indicating grouped or mapped regions within the assembly. As the grid extends toward the right and downward from row 2 to row 7, the cells from the right contain an asterisk instead of numbers. Each cell in rows 8 to 10 contains an asterisk. The numeric region gradually transitions into the asterisk-filled region, showing a partial assembly rather than a fully populated grid.

Overview of all five 2D unit-cell geometries with distinct fiber paths and filler layouts, and corresponding finite-element meshes, showing element sizing (matrix: 0.0045 mm, fiber: 0.0015 mm)

Figure 3
A schematic diagram shows patterned units mapped into an arrangement matrix and assembled into a larger grid.On the left, five square patterned tiles are shown with distinct fiber paths and circular fillers. “Unit‑1” appears in the top left and includes two semicircular, one curved, and one diagonal fiber path and two circular fillers. “Unit‑2” appears on the middle left and shows two main diagonal and two semicircular fibers crossing the tile with two circular fillers near opposite corners. “Unit‑3” appears at the bottom left and contains large curved fiber arcs near the top-right and bottom edges, with two circular fillers on the left. “Unit‑4” appears at the center and shows a central vertical fiber connected to two large curved fibers forming a U shape, with two circular fillers near the upper corners. “Unit‑5” appears below unit-4 and displays multiple intersecting curved fibers creating a network across the tile, with three circular fillers placed near the top left, center, and bottom right. Rightward arrows with numbers “1”, “2”, “3”, “4”, and “5” from these units indicate how these units are referenced. At the center is a rectangular numerical table labeled “Arrangement matrix n by m” below the grid. The matrix consists of ten rows and ten columns. Each cell contains a single integer value between 1 and 5. The numbers are evenly spaced and aligned, forming a clear grid without visible row or column headers. In the top-left corner of the matrix, the first row begins with the sequence “1, 3, 1, 5”, and the second row begins with “3, 2, 5, 4”. These initial cells are lightly shaded in different colors, visually distinguishing them from the rest of the table. The remaining cells are unshaded and contain only numeric characters on a white background. These numbers correspond to the unit labels shown on the left. Curved arrows above the matrix point from selected numbers in the matrix toward the right side of the figure. On the right, a larger grid labeled “Assembly n dot L times m dot L” shows an expanded layout. The grid is divided into ten evenly spaced rows and ten columns with visible cell borders. In the upper-left portion, several rows contain numeric values from 1 to 5 arranged in a structured pattern. In the first row, the cells contain “1, 3, 1, 5, 2, 4, 3, 5, 1, 2”, and in the second row, the cells contain “3, 2, 5, 4, 1, 2, 4, 3, 5, asterisk”, with the numeric cells lightly shaded in different colors, indicating grouped or mapped regions within the assembly. As the grid extends toward the right and downward from row 2 to row 7, the cells from the right contain an asterisk instead of numbers. Each cell in rows 8 to 10 contains an asterisk. The numeric region gradually transitions into the asterisk-filled region, showing a partial assembly rather than a fully populated grid.

Overview of all five 2D unit-cell geometries with distinct fiber paths and filler layouts, and corresponding finite-element meshes, showing element sizing (matrix: 0.0045 mm, fiber: 0.0015 mm)

Close modal
Figure 4
A schematic shows an arrangement matrix mapped into a patterned assembly image.The image is divided into two main panels arranged horizontally. On the left is a large rectangular grid labeled “Arrangement matrix 1”. The grid contains twenty rows and twenty columns filled with single-digit numbers from 1 to 5. The numbers are evenly spaced and aligned in a uniform matrix. All cells contain numeric values. An arrow points from the right edge of the numerical matrix toward the second panel. On the right is a square image labeled “Assembly 1”. This panel shows a continuous blue background filled with dense, repeating white curved line patterns. The pattern appears seamless across the entire square. The arrow visually indicates that the numerical arrangement in “Arrangement matrix 1” is used to generate or assemble the patterned surface shown in “Assembly 1”, linking the structured numeric grid to the final assembled pattern.

Arrangement matrix and the corresponding assembly

Figure 4
A schematic shows an arrangement matrix mapped into a patterned assembly image.The image is divided into two main panels arranged horizontally. On the left is a large rectangular grid labeled “Arrangement matrix 1”. The grid contains twenty rows and twenty columns filled with single-digit numbers from 1 to 5. The numbers are evenly spaced and aligned in a uniform matrix. All cells contain numeric values. An arrow points from the right edge of the numerical matrix toward the second panel. On the right is a square image labeled “Assembly 1”. This panel shows a continuous blue background filled with dense, repeating white curved line patterns. The pattern appears seamless across the entire square. The arrow visually indicates that the numerical arrangement in “Arrangement matrix 1” is used to generate or assemble the patterned surface shown in “Assembly 1”, linking the structured numeric grid to the final assembled pattern.

Arrangement matrix and the corresponding assembly

Close modal
Figure 5
A diagram shows an arrangement matrix with highlighted cells used to compute effective values from neighboring units.The image consists of three main parts arranged horizontally. On the left, a square patterned tile is labeled “Unit-1 P B C”, showing a single unit with a symmetric curved-line pattern. An arrow points from this unit toward its upper right, labeled “E superscript e f f”, indicating an effective value derived from surrounding units. In the center, a large square grid displays an arrangement matrix filled with numbers from 1 to 5. The grid is evenly divided into ten rows and ten columns. Three subregions are outlined in red squares, each enclosing a small block of cells: columns 2 to 4 of rows 2 to 4; columns 7 to 9 of rows 3 to 5; and columns 3 to 5 of rows 6 to 8. Within each red-outlined block, one central cell is shaded light green and contains the value “1”, indicating the focal unit. The surrounding cells within and around these blocks contain other numeric values from 2 to 5. On the right, three enlarged schematic diagrams correspond to selected highlighted cells from the matrix. Each schematic shows a central square labeled “1”, surrounded on all four sides and corners by numbers representing neighboring cells. Arrows point inward from the surrounding numbers toward the central “1”, illustrating how neighboring values contribute to an effective quantity. Each schematic is labeled with a different effective value name: “E superscript e f f-1”, “E superscript e f f-3”, and “E superscript e f f-2”. Dashed arrows connect specific highlighted cells in the central matrix to their corresponding schematic on the right. The row-wise numbers from the corresponding subregions are as follows: E superscript e f f-1, row 1: 2, 5, 4; row 2: 4, 1, 3; row 3: 2, 3, 4. E superscript e f f-3, row 1: 3, 2, 5; row 2: 2, 1, 4; row 3: 5, 4, 2. E superscript e f f-2, row 1: 5, 2, 3; row 2: 2, 1, 5; row 3: 5, 2, 3.

Illustration of the neighborhood influence on the unit cell. A target unit cell (shaded) is embedded in several distinct neighboring layouts composed of the same five canonical unit types, but arranged in different spatial patterns

Figure 5
A diagram shows an arrangement matrix with highlighted cells used to compute effective values from neighboring units.The image consists of three main parts arranged horizontally. On the left, a square patterned tile is labeled “Unit-1 P B C”, showing a single unit with a symmetric curved-line pattern. An arrow points from this unit toward its upper right, labeled “E superscript e f f”, indicating an effective value derived from surrounding units. In the center, a large square grid displays an arrangement matrix filled with numbers from 1 to 5. The grid is evenly divided into ten rows and ten columns. Three subregions are outlined in red squares, each enclosing a small block of cells: columns 2 to 4 of rows 2 to 4; columns 7 to 9 of rows 3 to 5; and columns 3 to 5 of rows 6 to 8. Within each red-outlined block, one central cell is shaded light green and contains the value “1”, indicating the focal unit. The surrounding cells within and around these blocks contain other numeric values from 2 to 5. On the right, three enlarged schematic diagrams correspond to selected highlighted cells from the matrix. Each schematic shows a central square labeled “1”, surrounded on all four sides and corners by numbers representing neighboring cells. Arrows point inward from the surrounding numbers toward the central “1”, illustrating how neighboring values contribute to an effective quantity. Each schematic is labeled with a different effective value name: “E superscript e f f-1”, “E superscript e f f-3”, and “E superscript e f f-2”. Dashed arrows connect specific highlighted cells in the central matrix to their corresponding schematic on the right. The row-wise numbers from the corresponding subregions are as follows: E superscript e f f-1, row 1: 2, 5, 4; row 2: 4, 1, 3; row 3: 2, 3, 4. E superscript e f f-3, row 1: 3, 2, 5; row 2: 2, 1, 4; row 3: 5, 4, 2. E superscript e f f-2, row 1: 5, 2, 3; row 2: 2, 1, 5; row 3: 5, 2, 3.

Illustration of the neighborhood influence on the unit cell. A target unit cell (shaded) is embedded in several distinct neighboring layouts composed of the same five canonical unit types, but arranged in different spatial patterns

Close modal
Figure 6
A pair of scatter plots shows “R subscript e” and “R subscript v” values versus geometry number.The figure contains two side-by-side scatter plots labeled “(a). Scatter plot-R e” on the left and “(b). Scatter plot-R v” on the right. Both plots use “Geometry Number” on the horizontal axis, ranging from 1 to 30 in increments of 5 units, with dashed gridlines across the background. In the left plot, the vertical axis is labeled “R subscript e”, ranging from 0.8 to 1.2 with an interval of 0.2. Two datasets are shown: the circular markers labeled “R subscript e superscript 22” and the square markers labeled “R subscript e superscript 11”, as indicated by the legend in the upper right of the plot. The data points are distributed around a horizontal value near 1.0. The circular points show a wider spread, extending roughly from about 0.87 to 1.15, while the squares are more tightly clustered close to 1.0 across all geometry numbers. In the right plot, the vertical axis is labeled “R subscript v”, ranging from 0.6 to 1.3 with an interval of 0.1. The square markers represent the data, with a legend entry labeled “R subscript v” near the top right. The values span approximately from 0.78 to 1.25, with most points clustered around 1.0. The scatter shows variability across geometry numbers without a clearly drawn trend line. Note: All the numerical data values are approximated.

Scatter plot of local-neighbor effect ratios across randomly selected unit-cell samples

Figure 6
A pair of scatter plots shows “R subscript e” and “R subscript v” values versus geometry number.The figure contains two side-by-side scatter plots labeled “(a). Scatter plot-R e” on the left and “(b). Scatter plot-R v” on the right. Both plots use “Geometry Number” on the horizontal axis, ranging from 1 to 30 in increments of 5 units, with dashed gridlines across the background. In the left plot, the vertical axis is labeled “R subscript e”, ranging from 0.8 to 1.2 with an interval of 0.2. Two datasets are shown: the circular markers labeled “R subscript e superscript 22” and the square markers labeled “R subscript e superscript 11”, as indicated by the legend in the upper right of the plot. The data points are distributed around a horizontal value near 1.0. The circular points show a wider spread, extending roughly from about 0.87 to 1.15, while the squares are more tightly clustered close to 1.0 across all geometry numbers. In the right plot, the vertical axis is labeled “R subscript v”, ranging from 0.6 to 1.3 with an interval of 0.1. The square markers represent the data, with a legend entry labeled “R subscript v” near the top right. The values span approximately from 0.78 to 1.25, with most points clustered around 1.0. The scatter shows variability across geometry numbers without a clearly drawn trend line. Note: All the numerical data values are approximated.

Scatter plot of local-neighbor effect ratios across randomly selected unit-cell samples

Close modal
Figure 7
A diagram shows an arrangement matrix with padding and extracted local geometry matrices.The image illustrates how local geometry matrices are extracted from an arrangement matrix using padding. On the left, a large grid labeled “Arrangement matrix” contains rows and columns filled with numbers from 1 to 5. The matrix is surrounded on the top two rows and left two columns by a green shaded region filled with zeros, identified as the padding area. The zeros extend beyond the visible numeric grid, indicating boundary padding. Five five-by-five neighborhoods within the arrangement matrix are highlighted using colored rectangular outlines: columns 1 to 5 of rows 1 to 5; columns 2 to 6 of rows 1 to 5; columns 3 to 7 of rows 1 to 5; columns 1 to 5 of rows 2 to 6; and columns 8 to 12 of rows 8 to 12. Inside these outlines, one central cell is emphasized with a light background color, marking the focal value. Red arrows above some highlighted cells indicate horizontal movement or indexing across adjacent cells. Different highlighted regions correspond to different focal positions within the matrix, including positions near the padded boundaries and positions fully inside the matrix. On the right side, four smaller square grids, with an ellipsis, are shown under the label “Extracted local geometry matrices”. Each small grid represents a local five-by-five matrix extracted from the larger arrangement matrix. Three of these local matrices include green-shaded rows or columns of zeros, showing how padding values are incorporated when the focal cell lies near the boundary. In each extracted matrix, the central cell is highlighted and contains a value such as “1” in the first, “3” in the second, “4” in the third, and “5” in the fourth, while the surrounding cells display neighboring values taken from the arrangement matrix or zeros from the padding area. Arrows connect selected highlighted regions in the arrangement matrix to their corresponding extracted local geometry matrices. The row-wise numbers from the corresponding matrices are as follows: First matrix, row 1: 0, 0, 0, 0, 0; row 2: 0, 0, 0, 0, 0; row 3: 0, 0, 1, 3, 4; row 4: 0, 0, 3, 2, 5; row 5: 0, 0, 2, 4, 1. Second matrix, row 1: 0, 0, 0, 0, 0; row 2: 0, 0, 0, 0, 0; row 3: 0, 1, 3, 4, 5; row 4: 0, 3, 2, 5, 4; row 5: 0, 2, 4, 1, 3. Third matrix, row 1: 0, 0, 0, 0, 0; row 2: 0, 0, 0, 0, 0; row 3: 1, 3, 4, 5, 2; row 4: 3, 2, 5, 4, 1; row 5: 2, 4, 1, 3, 4. Fourth matrix, row 1: 5, 2, 3, 2, 5; row 2: 1, 4, 2, 1, 3; row 3: 3, 1, 5, 4, 2; row 4: 5, 2, 4, 2, 1; row 5: 2, 1, 3, 5, 2.

Illustration of the sliding-window extraction process used to generate local 5 × 5 geometry matrices from a larger arrangement. A 5 × 5 window is moved across the full arrangement matrix (padding boundary cases), and at each position, the centered unit cell and its first- and second-layer neighbors are captured as a distinct input sample for the neural network

Figure 7
A diagram shows an arrangement matrix with padding and extracted local geometry matrices.The image illustrates how local geometry matrices are extracted from an arrangement matrix using padding. On the left, a large grid labeled “Arrangement matrix” contains rows and columns filled with numbers from 1 to 5. The matrix is surrounded on the top two rows and left two columns by a green shaded region filled with zeros, identified as the padding area. The zeros extend beyond the visible numeric grid, indicating boundary padding. Five five-by-five neighborhoods within the arrangement matrix are highlighted using colored rectangular outlines: columns 1 to 5 of rows 1 to 5; columns 2 to 6 of rows 1 to 5; columns 3 to 7 of rows 1 to 5; columns 1 to 5 of rows 2 to 6; and columns 8 to 12 of rows 8 to 12. Inside these outlines, one central cell is emphasized with a light background color, marking the focal value. Red arrows above some highlighted cells indicate horizontal movement or indexing across adjacent cells. Different highlighted regions correspond to different focal positions within the matrix, including positions near the padded boundaries and positions fully inside the matrix. On the right side, four smaller square grids, with an ellipsis, are shown under the label “Extracted local geometry matrices”. Each small grid represents a local five-by-five matrix extracted from the larger arrangement matrix. Three of these local matrices include green-shaded rows or columns of zeros, showing how padding values are incorporated when the focal cell lies near the boundary. In each extracted matrix, the central cell is highlighted and contains a value such as “1” in the first, “3” in the second, “4” in the third, and “5” in the fourth, while the surrounding cells display neighboring values taken from the arrangement matrix or zeros from the padding area. Arrows connect selected highlighted regions in the arrangement matrix to their corresponding extracted local geometry matrices. The row-wise numbers from the corresponding matrices are as follows: First matrix, row 1: 0, 0, 0, 0, 0; row 2: 0, 0, 0, 0, 0; row 3: 0, 0, 1, 3, 4; row 4: 0, 0, 3, 2, 5; row 5: 0, 0, 2, 4, 1. Second matrix, row 1: 0, 0, 0, 0, 0; row 2: 0, 0, 0, 0, 0; row 3: 0, 1, 3, 4, 5; row 4: 0, 3, 2, 5, 4; row 5: 0, 2, 4, 1, 3. Third matrix, row 1: 0, 0, 0, 0, 0; row 2: 0, 0, 0, 0, 0; row 3: 1, 3, 4, 5, 2; row 4: 3, 2, 5, 4, 1; row 5: 2, 4, 1, 3, 4. Fourth matrix, row 1: 5, 2, 3, 2, 5; row 2: 1, 4, 2, 1, 3; row 3: 3, 1, 5, 4, 2; row 4: 5, 2, 4, 2, 1; row 5: 2, 1, 3, 5, 2.

Illustration of the sliding-window extraction process used to generate local 5 × 5 geometry matrices from a larger arrangement. A 5 × 5 window is moved across the full arrangement matrix (padding boundary cases), and at each position, the centered unit cell and its first- and second-layer neighbors are captured as a distinct input sample for the neural network

Close modal
Figure 8
A set of five colored image tiles shows patterned regions with R G B values mapped to material types.The diagram displays five separate square tiles representing composite material microstructures. Each tile contains a dark blue background region labeled “R G B relates to matrix region”, curved yellow bands labeled “R G B relates to fiber region”, and circular teal inclusions labeled “R G B relates to filler region”. Each tile has a vertical color bar on its right side, showing a continuous gradient from dark blue through green to yellow. The patterns differ slightly from tile to tile, with changes in the orientation and curvature of the yellow bands and the placement of the teal circles. The background remains consistently dark blue across all tiles. The tile on the top left includes two semicircular, one curved, and one diagonal fiber path and two circular fillers. The tile on the top center shows two main diagonal and two semicircular fibers crossing the tile with two circular fillers near opposite corners. The tile on the top right contains large curved fiber arcs near the top-right and bottom edges, with two circular fillers on the left. The tile at the bottom left shows a central vertical fiber connected to two large curved fibers forming a U shape, with two circular fillers near the upper corners. The tile at the bottom right displays multiple intersecting curved fibers, creating a network across the tile, with three circular fillers placed near the top left, center, and bottom right.

Segmentation of finite-element simulation images into phase-specific regions. Each color in the RGB image uniquely represents one of the internal material phases: matrix, fiber, or filler. These segmented regions were then translated into numerical values based on the mechanical properties of each phase, forming the foundation of the unit cell's feature matrix

Figure 8
A set of five colored image tiles shows patterned regions with R G B values mapped to material types.The diagram displays five separate square tiles representing composite material microstructures. Each tile contains a dark blue background region labeled “R G B relates to matrix region”, curved yellow bands labeled “R G B relates to fiber region”, and circular teal inclusions labeled “R G B relates to filler region”. Each tile has a vertical color bar on its right side, showing a continuous gradient from dark blue through green to yellow. The patterns differ slightly from tile to tile, with changes in the orientation and curvature of the yellow bands and the placement of the teal circles. The background remains consistently dark blue across all tiles. The tile on the top left includes two semicircular, one curved, and one diagonal fiber path and two circular fillers. The tile on the top center shows two main diagonal and two semicircular fibers crossing the tile with two circular fillers near opposite corners. The tile on the top right contains large curved fiber arcs near the top-right and bottom edges, with two circular fillers on the left. The tile at the bottom left shows a central vertical fiber connected to two large curved fibers forming a U shape, with two circular fillers near the upper corners. The tile at the bottom right displays multiple intersecting curved fibers, creating a network across the tile, with three circular fillers placed near the top left, center, and bottom right.

Segmentation of finite-element simulation images into phase-specific regions. Each color in the RGB image uniquely represents one of the internal material phases: matrix, fiber, or filler. These segmented regions were then translated into numerical values based on the mechanical properties of each phase, forming the foundation of the unit cell's feature matrix

Close modal
Figure 9
A figure shows a convolutional neural network architecture from input through convolutional layers to fully connected output.The diagram illustrates the structure of a convolutional neural network from left to right. On the far left, a yellow block labeled “input 2 by 500 by 500” represents a two-channel input image of size 500 by 500. An arrow leads to the first convolutional stage labeled “Convolutional layer 1, Block pooling”, shown as a stack of green feature maps labeled “256 filter”. This output passes through a R e L U activation and is annotated as “256 by 5 by 5”. The network then enters a grouped section labeled “Convolutional layers 2–6”. Within this section, multiple stacks of purple feature maps are shown, labeled sequentially with decreasing numbers of filters: “128 filter”, “64 filter”, “32 filter”, “16 filter”, and “8 filter”. A small orange square labeled “3 by 3 kernel” indicates the kernel size used in these convolutional layers. The final convolutional output is annotated as “8 by 5 by 5” followed by “R e L U”. After the convolutional stages, the feature maps are flattened, indicated by the label “Flatten”, and passed into a fully connected neural network arranged from left to right. On the left, a large group of circular nodes represents the first hidden layer, labeled with “R e L U” above it and annotated below as having “512 neurons”. Each node in this layer is connected by lines to every node in the next layer. The second hidden layer is shown to the right, also labeled “R e L U”, and is annotated below as having “256 neurons”. Dense connection lines link all neurons from the previous layer to this layer. The third hidden layer follows, again labeled “R e L U”, with “64 neurons” indicated below. As before, all neurons are fully connected to the next stage. On the far right, a small output layer contains two circular nodes, labeled “output 2 neurons”. Lines connect every neuron in the final hidden layer to both output neurons. Dotted vertical ellipses beneath each hidden layer indicate that the illustrated nodes represent larger groups of neurons rather than every individual unit being drawn.

Architecture of the lightweight CNN model used for predicting local property ratios

Figure 9
A figure shows a convolutional neural network architecture from input through convolutional layers to fully connected output.The diagram illustrates the structure of a convolutional neural network from left to right. On the far left, a yellow block labeled “input 2 by 500 by 500” represents a two-channel input image of size 500 by 500. An arrow leads to the first convolutional stage labeled “Convolutional layer 1, Block pooling”, shown as a stack of green feature maps labeled “256 filter”. This output passes through a R e L U activation and is annotated as “256 by 5 by 5”. The network then enters a grouped section labeled “Convolutional layers 2–6”. Within this section, multiple stacks of purple feature maps are shown, labeled sequentially with decreasing numbers of filters: “128 filter”, “64 filter”, “32 filter”, “16 filter”, and “8 filter”. A small orange square labeled “3 by 3 kernel” indicates the kernel size used in these convolutional layers. The final convolutional output is annotated as “8 by 5 by 5” followed by “R e L U”. After the convolutional stages, the feature maps are flattened, indicated by the label “Flatten”, and passed into a fully connected neural network arranged from left to right. On the left, a large group of circular nodes represents the first hidden layer, labeled with “R e L U” above it and annotated below as having “512 neurons”. Each node in this layer is connected by lines to every node in the next layer. The second hidden layer is shown to the right, also labeled “R e L U”, and is annotated below as having “256 neurons”. Dense connection lines link all neurons from the previous layer to this layer. The third hidden layer follows, again labeled “R e L U”, with “64 neurons” indicated below. As before, all neurons are fully connected to the next stage. On the far right, a small output layer contains two circular nodes, labeled “output 2 neurons”. Lines connect every neuron in the final hidden layer to both output neurons. Dotted vertical ellipses beneath each hidden layer indicate that the illustrated nodes represent larger groups of neurons rather than every individual unit being drawn.

Architecture of the lightweight CNN model used for predicting local property ratios

Close modal
Figure 10
A multi-panel figure shows loss and R-squared training curves for three machine learning models.The figure contains six line plots arranged in three rows and two columns, labeled (a) through (f). All plots use “Epoch” on the horizontal axis. The left-column plots show mean squared error with the vertical axis labeled “M S E”, and the right-column plots show coefficient of determination with the vertical axis labeled “R-squared”. Each plot in the left column includes two curves: a line with the square markers labeled “Train loss” and a line with the circular markers labeled “Validation loss”. Each plot in the right column includes two curves: a line with the square markers labeled “Train R-squared” and a line with the circular markers labeled “Validation R-squared”. Light dashed gridlines appear in the background of all panels. Panel (a), titled “Loss curve of lightweight model”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from 0.00 to 0.16 with an interval of 0.02. It shows training M S E, starting from 0.148, and validation M S E, starting from 0.068, decreasing rapidly during the early epochs and then gradually leveling off at low values by around 120 epochs. The validation loss follows a similar trend with small fluctuations. Panel (b), titled “R-squared curve of lightweight model”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from negative 10 to 2 with an interval of 2. It shows training R-squared, starting from negative 8.3, and validation R-squared, starting from negative 1, increasing at early epochs toward values near 1 as epochs increase, with validation R-squared showing slight oscillations. Panel (c), titled “Loss curve of Model-1”: The horizontal axis ranges from 0 to 100 with an interval of 20, and the vertical axis ranges from 0.00 to 0.07 with an interval of 0.01. It shows training M S E, starting from 0.07, and validation M S E, starting from 0.015, steadily decreasing toward near-zero values by about 100 epochs. Panel (d), titled “R-squared curve of Model-1”: The horizontal axis ranges from 0 to 100 with an interval of 20, and the vertical axis ranges from negative 6 to 2 with an interval of 2. It shows R-squared rising from negative values toward positive values close to 1, with validation R-squared fluctuating slightly above the training curve. Panel (e), titled “Loss curve of Model-2”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from 0.00 to 0.06 with an interval of 0.01. It shows training M S E, starting from 0.055, and validation M S E, starting from 0.005, decreasing quickly at first and then tapering to very small values by around 120 epochs, with validation loss remaining consistently low. Panel (f), titled “R-squared curve of Model-2”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from negative 5 to 2 with an interval of 1. It shows training and validation R-squared increasing from negative 5 and 0, respectively, and converging toward values close to 1 as training progresses. Note: All the numerical data values are approximated.

Architecture of the enhanced CNN model used for predicting local property ratios

Figure 10
A multi-panel figure shows loss and R-squared training curves for three machine learning models.The figure contains six line plots arranged in three rows and two columns, labeled (a) through (f). All plots use “Epoch” on the horizontal axis. The left-column plots show mean squared error with the vertical axis labeled “M S E”, and the right-column plots show coefficient of determination with the vertical axis labeled “R-squared”. Each plot in the left column includes two curves: a line with the square markers labeled “Train loss” and a line with the circular markers labeled “Validation loss”. Each plot in the right column includes two curves: a line with the square markers labeled “Train R-squared” and a line with the circular markers labeled “Validation R-squared”. Light dashed gridlines appear in the background of all panels. Panel (a), titled “Loss curve of lightweight model”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from 0.00 to 0.16 with an interval of 0.02. It shows training M S E, starting from 0.148, and validation M S E, starting from 0.068, decreasing rapidly during the early epochs and then gradually leveling off at low values by around 120 epochs. The validation loss follows a similar trend with small fluctuations. Panel (b), titled “R-squared curve of lightweight model”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from negative 10 to 2 with an interval of 2. It shows training R-squared, starting from negative 8.3, and validation R-squared, starting from negative 1, increasing at early epochs toward values near 1 as epochs increase, with validation R-squared showing slight oscillations. Panel (c), titled “Loss curve of Model-1”: The horizontal axis ranges from 0 to 100 with an interval of 20, and the vertical axis ranges from 0.00 to 0.07 with an interval of 0.01. It shows training M S E, starting from 0.07, and validation M S E, starting from 0.015, steadily decreasing toward near-zero values by about 100 epochs. Panel (d), titled “R-squared curve of Model-1”: The horizontal axis ranges from 0 to 100 with an interval of 20, and the vertical axis ranges from negative 6 to 2 with an interval of 2. It shows R-squared rising from negative values toward positive values close to 1, with validation R-squared fluctuating slightly above the training curve. Panel (e), titled “Loss curve of Model-2”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from 0.00 to 0.06 with an interval of 0.01. It shows training M S E, starting from 0.055, and validation M S E, starting from 0.005, decreasing quickly at first and then tapering to very small values by around 120 epochs, with validation loss remaining consistently low. Panel (f), titled “R-squared curve of Model-2”: The horizontal axis ranges from 0 to 120 with an interval of 20, and the vertical axis ranges from negative 5 to 2 with an interval of 1. It shows training and validation R-squared increasing from negative 5 and 0, respectively, and converging toward values close to 1 as training progresses. Note: All the numerical data values are approximated.

Architecture of the enhanced CNN model used for predicting local property ratios

Close modal
Figure 11
Two scatter plots compare predicted and ground truth values for “R subscript e” and “R subscript v” across three models.The figure contains two side-by-side scatter plots labeled “(a). Predicted R e versus ground truth values” on the left and “(b). Predicted R v versus ground truth values” on the right. In both plots, three datasets are shown using different markers, as indicated by the legend in the upper left: the squares labeled “Model-1”, the circles labeled “Model-2”, and the triangles labeled “Lightweight model”. In the left plot, the vertical axis is labeled “Predicted R subscript e”, ranging from 0.80 to 1.20 with an interval of 0.05. The horizontal axis is labeled “Ground Truth R subscript e”, ranging from 0.80 to 1.20 with an interval of 0.05. The data points form a dense diagonal band from the lower left at (0.83, 0.82) to the upper right at (1.18, 1.18), indicating that predicted values closely follow the ground truth across the range. In the right plot, the vertical axis is labeled “Predicted R subscript v”, ranging from 0.80 to 1.20 with an interval of 0.05. The horizontal axis is labeled “Ground Truth R subscript v”, ranging from 0.80 to 1.20 with an interval of 0.05. The points again align along a diagonal trend from about (0.83, 0.78) to (1.18, 1.21), showing similar agreement between predicted and ground truth values for “R subscript v”. Note: All the numerical data values are approximated.

Scatter plots comparing predicted values of Re and Rν against their respective ground truth values from the validation dataset

Figure 11
Two scatter plots compare predicted and ground truth values for “R subscript e” and “R subscript v” across three models.The figure contains two side-by-side scatter plots labeled “(a). Predicted R e versus ground truth values” on the left and “(b). Predicted R v versus ground truth values” on the right. In both plots, three datasets are shown using different markers, as indicated by the legend in the upper left: the squares labeled “Model-1”, the circles labeled “Model-2”, and the triangles labeled “Lightweight model”. In the left plot, the vertical axis is labeled “Predicted R subscript e”, ranging from 0.80 to 1.20 with an interval of 0.05. The horizontal axis is labeled “Ground Truth R subscript e”, ranging from 0.80 to 1.20 with an interval of 0.05. The data points form a dense diagonal band from the lower left at (0.83, 0.82) to the upper right at (1.18, 1.18), indicating that predicted values closely follow the ground truth across the range. In the right plot, the vertical axis is labeled “Predicted R subscript v”, ranging from 0.80 to 1.20 with an interval of 0.05. The horizontal axis is labeled “Ground Truth R subscript v”, ranging from 0.80 to 1.20 with an interval of 0.05. The points again align along a diagonal trend from about (0.83, 0.78) to (1.18, 1.21), showing similar agreement between predicted and ground truth values for “R subscript v”. Note: All the numerical data values are approximated.

Scatter plots comparing predicted values of Re and Rν against their respective ground truth values from the validation dataset

Close modal
Figure 12
A set of five line plots shows stress–strain curves comparing original and homogenized units.The figure consists of five separate stress–strain plots arranged in a grid layout, each corresponding to a different unit labeled “Original unit-1” through “Original unit-5”, with a matching curve labeled “Homogenized unit-1” through “Homogenized unit-5”. Each subplot has the horizontal axis labeled “Strain”, ranging from 0.000 to 0.025 with an interval of 0.005, and the vertical axis labeled “Stress (Megapascals)”, ranging from 0 to 3000 with an interval of 500. In each plot, two curves are shown with markers connected by lines. The “Original unit” curve is plotted with the square markers, while the “Homogenized unit” curve is plotted with the circular markers. Both curves start near zero stress at zero strain and increase nonlinearly as strain increases. Across all five units, the stress rises steeply at low strain, then gradually levels off at higher strain values. In the top left plot, the line for “Original unit-1” increases to (0.009, 1750), then levels off at (0.0225, 2050), and the line for “Homogenized unit-1” increases to (0.0115, 1750), then levels off at (0.0225, 2100). In the top right plot, the line for “Original unit-2” increases to (0.015, 2100), then levels off at (0.0225, 2200), and the line for “Homogenized unit-2” increases to (0.015, 2100), then levels off at (0.0225, 2350). In the middle left plot, the line for “Original unit-3” increases to (0.015, 2100), then levels off at (0.0225, 2200), and the line for “Homogenized unit-3” increases to (0.015, 2100), then levels off at (0.0225, 2350). In the middle right plot, the line for “Original unit-4” increases to (0.0125, 2250), then levels off at (0.0225, 2300), and the line for “Homogenized unit-4” increases to (0.015, 2250), then levels off at (0.0225, 2350). In the bottom left plot, the line for “Original unit-5” increases to (0.0135, 1750), then levels off at (0.0225, 1800), and the line for “Homogenized unit-5” increases to (0.0135, 1750), then levels off at (0.0225, 1900). Each subplot includes a legend identifying the two curves for that unit, and light dashed gridlines are visible in the background. Note: All the numerical data values are approximated.

Comparison of equivalent stress–strain curves obtained from the homogenized unit cell responses and those derived from full-fidelity finite element simulations

Figure 12
A set of five line plots shows stress–strain curves comparing original and homogenized units.The figure consists of five separate stress–strain plots arranged in a grid layout, each corresponding to a different unit labeled “Original unit-1” through “Original unit-5”, with a matching curve labeled “Homogenized unit-1” through “Homogenized unit-5”. Each subplot has the horizontal axis labeled “Strain”, ranging from 0.000 to 0.025 with an interval of 0.005, and the vertical axis labeled “Stress (Megapascals)”, ranging from 0 to 3000 with an interval of 500. In each plot, two curves are shown with markers connected by lines. The “Original unit” curve is plotted with the square markers, while the “Homogenized unit” curve is plotted with the circular markers. Both curves start near zero stress at zero strain and increase nonlinearly as strain increases. Across all five units, the stress rises steeply at low strain, then gradually levels off at higher strain values. In the top left plot, the line for “Original unit-1” increases to (0.009, 1750), then levels off at (0.0225, 2050), and the line for “Homogenized unit-1” increases to (0.0115, 1750), then levels off at (0.0225, 2100). In the top right plot, the line for “Original unit-2” increases to (0.015, 2100), then levels off at (0.0225, 2200), and the line for “Homogenized unit-2” increases to (0.015, 2100), then levels off at (0.0225, 2350). In the middle left plot, the line for “Original unit-3” increases to (0.015, 2100), then levels off at (0.0225, 2200), and the line for “Homogenized unit-3” increases to (0.015, 2100), then levels off at (0.0225, 2350). In the middle right plot, the line for “Original unit-4” increases to (0.0125, 2250), then levels off at (0.0225, 2300), and the line for “Homogenized unit-4” increases to (0.015, 2250), then levels off at (0.0225, 2350). In the bottom left plot, the line for “Original unit-5” increases to (0.0135, 1750), then levels off at (0.0225, 1800), and the line for “Homogenized unit-5” increases to (0.0135, 1750), then levels off at (0.0225, 1900). Each subplot includes a legend identifying the two curves for that unit, and light dashed gridlines are visible in the background. Note: All the numerical data values are approximated.

Comparison of equivalent stress–strain curves obtained from the homogenized unit cell responses and those derived from full-fidelity finite element simulations

Close modal
Figure 13
A six-panel heatmap compares generated index values from a lightweight model, Model-1, and Model-2.The figure contains six square heatmaps arranged in a three-by-two grid. All heatmaps use “Index” on both the horizontal and vertical axes, with index values running from 1 to 20. Each heatmap includes a vertical color bar on the right side showing percentage ranges, labeled from “68 percent to about 72 percent” at the bottom through “72 percent to about 76 percent”, “76 percent to about 81 percent”, “81 percent to about 85 percent”, “85 percent to about 89 percent”, up to “greater than 89 percent” at the top. The color scale transitions from blue at lower percentages to green and yellow at higher percentages. The color bars in the left column are labeled “I subscript e”, and those in the right column are labeled “I subscript v”. The top row is labeled “(a). Heatmap of I generated by lightweight model”. Both heatmaps in this row show a dense mosaic dominated by green cells, with scattered yellow cells indicating higher percentage values and occasional blue cells indicating lower percentage values. The spatial distribution appears relatively uniform across the 20-by-20 grid, with no obvious directional pattern. The middle row is labeled “(b). Heatmap of I generated by model-1”. The two heatmaps again show predominantly green regions with intermittent yellow and blue cells. Compared with row (a), some individual cells appear brighter yellow or darker blue, but the overall distribution remains evenly spread across indices. In the left heatmap, the cells at (5, 16), (7, 9), and (15, 15) are in white, while in the right one, the cells at (10, 3), (13, 13), and (14, 5) are in white. The bottom row is labeled “(c). Heatmap of I generated by model-2”. These heatmaps also follow the same layout and color scale. The grids show similar mixtures of green, yellow, and blue cells, with most values falling in the mid-to-high percentage ranges and a small number of lower-percentage cells dispersed throughout. In the left heatmap, a cell at (9, 12) is in white, while in the right one, a cell at (17, 13) is in white. Note: All the numerical data values are approximated.

Heatmap visualization of the improvement ratio, i.e. and Iν, representing the reduction in effective stiffness homogenization error due to neural network correction

Figure 13
A six-panel heatmap compares generated index values from a lightweight model, Model-1, and Model-2.The figure contains six square heatmaps arranged in a three-by-two grid. All heatmaps use “Index” on both the horizontal and vertical axes, with index values running from 1 to 20. Each heatmap includes a vertical color bar on the right side showing percentage ranges, labeled from “68 percent to about 72 percent” at the bottom through “72 percent to about 76 percent”, “76 percent to about 81 percent”, “81 percent to about 85 percent”, “85 percent to about 89 percent”, up to “greater than 89 percent” at the top. The color scale transitions from blue at lower percentages to green and yellow at higher percentages. The color bars in the left column are labeled “I subscript e”, and those in the right column are labeled “I subscript v”. The top row is labeled “(a). Heatmap of I generated by lightweight model”. Both heatmaps in this row show a dense mosaic dominated by green cells, with scattered yellow cells indicating higher percentage values and occasional blue cells indicating lower percentage values. The spatial distribution appears relatively uniform across the 20-by-20 grid, with no obvious directional pattern. The middle row is labeled “(b). Heatmap of I generated by model-1”. The two heatmaps again show predominantly green regions with intermittent yellow and blue cells. Compared with row (a), some individual cells appear brighter yellow or darker blue, but the overall distribution remains evenly spread across indices. In the left heatmap, the cells at (5, 16), (7, 9), and (15, 15) are in white, while in the right one, the cells at (10, 3), (13, 13), and (14, 5) are in white. The bottom row is labeled “(c). Heatmap of I generated by model-2”. These heatmaps also follow the same layout and color scale. The grids show similar mixtures of green, yellow, and blue cells, with most values falling in the mid-to-high percentage ranges and a small number of lower-percentage cells dispersed throughout. In the left heatmap, a cell at (9, 12) is in white, while in the right one, a cell at (17, 13) is in white. Note: All the numerical data values are approximated.

Heatmap visualization of the improvement ratio, i.e. and Iν, representing the reduction in effective stiffness homogenization error due to neural network correction

Close modal
Figure 14
A comparison figure shows stress and strain contour maps from full fidelity, lightweight, and homogenized models.The figure is arranged in two rows and three columns, comparing results from three modeling approaches labeled at the top as “Full fidelity result”, “Lightweight model informed”, and “Standard homogenization”. Each column corresponds to one approach. The top row, labeled “(a). Part Von-mises stress distribution of structure 27” shows color contour maps of Von Mises stress. Each map includes a vertical color bar on the right with units noted as “Megapascals”. In the full fidelity result, the stress field appears highly detailed, with complex curved patterns and multiple localized high-stress regions highlighted by dashed red circles. The color scale ranges from low values in blue (35.39) to high values in yellow and red (370.20). In the lightweight model informed result, the stress distribution is smoother and more averaged but still shows concentrated high-stress zones at locations corresponding to the full fidelity result, also marked by dashed red circles. The color scale ranges from 15.91 to 20.08. In the standard homogenization result, the stress field is even smoother, with fewer spatial details and broader stress regions, while still indicating similar general locations of higher stress. The color scale ranges from 10.42 to 19.08. The bottom row, labeled “(b). Part strain distribution of structure 27,” shows corresponding strain contour maps. Each plot includes a vertical color bar with values expressed as percentages, ranging approximately from about 0.87 percent for the left plot and 0.89 percent for the other two plots to 1.00 percent. The full fidelity strain map shows fine-scale variations and detailed patterns across the structure. The lightweight model-informed strain map presents smoother contours that retain the main strain concentration regions seen in the full fidelity case. The standard homogenization strain map is the smoothest, with reduced local variation and more uniform strain regions.

Comparison of stress and strain distributions in (left panel) the detailed heterogeneous model and (right panel) the homogenized model. The heterogeneous model exhibits localized variations due to fiber–matrix interfaces, while the homogenized model displays a smooth distribution consistent with the effective material properties

Figure 14
A comparison figure shows stress and strain contour maps from full fidelity, lightweight, and homogenized models.The figure is arranged in two rows and three columns, comparing results from three modeling approaches labeled at the top as “Full fidelity result”, “Lightweight model informed”, and “Standard homogenization”. Each column corresponds to one approach. The top row, labeled “(a). Part Von-mises stress distribution of structure 27” shows color contour maps of Von Mises stress. Each map includes a vertical color bar on the right with units noted as “Megapascals”. In the full fidelity result, the stress field appears highly detailed, with complex curved patterns and multiple localized high-stress regions highlighted by dashed red circles. The color scale ranges from low values in blue (35.39) to high values in yellow and red (370.20). In the lightweight model informed result, the stress distribution is smoother and more averaged but still shows concentrated high-stress zones at locations corresponding to the full fidelity result, also marked by dashed red circles. The color scale ranges from 15.91 to 20.08. In the standard homogenization result, the stress field is even smoother, with fewer spatial details and broader stress regions, while still indicating similar general locations of higher stress. The color scale ranges from 10.42 to 19.08. The bottom row, labeled “(b). Part strain distribution of structure 27,” shows corresponding strain contour maps. Each plot includes a vertical color bar with values expressed as percentages, ranging approximately from about 0.87 percent for the left plot and 0.89 percent for the other two plots to 1.00 percent. The full fidelity strain map shows fine-scale variations and detailed patterns across the structure. The lightweight model-informed strain map presents smoother contours that retain the main strain concentration regions seen in the full fidelity case. The standard homogenization strain map is the smoothest, with reduced local variation and more uniform strain regions.

Comparison of stress and strain distributions in (left panel) the detailed heterogeneous model and (right panel) the homogenized model. The heterogeneous model exhibits localized variations due to fiber–matrix interfaces, while the homogenized model displays a smooth distribution consistent with the effective material properties

Close modal
Figure 15
A line chart shows stress–strain curves comparing full fidelity, model-informed, lightweight, and homogenization methods.The chart plots “Stress (Megapascals)” on the vertical axis versus “Strain” on the horizontal axis. The strain axis ranges from 0.000 to about 0.012 with an interval of 0.002, and the stress axis ranges from 0 to 2500 megapascals with an interval of 500. Five curves are shown with distinct markers, identified by the legend. The square-marked curve labeled “Full fidelity” increases rapidly at low strain and then gradually levels off, reaching around 2000 megapascals near a strain of 0.010. The circle-marked curve labeled “Model-1 informed” follows a similar trend, closely tracking the full-fidelity curve and reaching slightly above 2100 megapascals at higher strain. The triangle-marked curve labeled “Model-2 informed” also closely follows the full-fidelity response and reaches slightly higher stress values than Model-1 informed at larger strains. The inverted triangle-marked curve labeled “Lightweight model” rises steeply and attains the highest stress among the model-based curves at higher strain, approaching roughly 2300 megapascals near a strain of 0.01. In contrast, the diamond-marked curve labeled “Standard homogenization” increases more gradually and remains lower than the other curves across the entire strain range, reaching around 1750 megapascals at the highest strain shown. All curves start near zero stress at zero strain and exhibit nonlinear behavior, with steeper slopes at low strain and reduced slopes at higher strain. Note: All the numerical data values are approximated.

Comparison of equivalent stress–strain curves obtained from the neural network-predicted homogenized unit cell responses and those derived from full-fidelity finite element simulations

Figure 15
A line chart shows stress–strain curves comparing full fidelity, model-informed, lightweight, and homogenization methods.The chart plots “Stress (Megapascals)” on the vertical axis versus “Strain” on the horizontal axis. The strain axis ranges from 0.000 to about 0.012 with an interval of 0.002, and the stress axis ranges from 0 to 2500 megapascals with an interval of 500. Five curves are shown with distinct markers, identified by the legend. The square-marked curve labeled “Full fidelity” increases rapidly at low strain and then gradually levels off, reaching around 2000 megapascals near a strain of 0.010. The circle-marked curve labeled “Model-1 informed” follows a similar trend, closely tracking the full-fidelity curve and reaching slightly above 2100 megapascals at higher strain. The triangle-marked curve labeled “Model-2 informed” also closely follows the full-fidelity response and reaches slightly higher stress values than Model-1 informed at larger strains. The inverted triangle-marked curve labeled “Lightweight model” rises steeply and attains the highest stress among the model-based curves at higher strain, approaching roughly 2300 megapascals near a strain of 0.01. In contrast, the diamond-marked curve labeled “Standard homogenization” increases more gradually and remains lower than the other curves across the entire strain range, reaching around 1750 megapascals at the highest strain shown. All curves start near zero stress at zero strain and exhibit nonlinear behavior, with steeper slopes at low strain and reduced slopes at higher strain. Note: All the numerical data values are approximated.

Comparison of equivalent stress–strain curves obtained from the neural network-predicted homogenized unit cell responses and those derived from full-fidelity finite element simulations

Close modal
Table 1

Material properties used in simulations

PropertiesPP matrixRubber fillerCarbon fiber
Constitutive modelSmall-strain isotropic elastic–plasticIsotropic linear elasticEngineering constants
E  (MPa)1,70030
ν0.40.47
E1  (MPa)135,000
E2  (MPa)7,000
G12  (MPa)4,000
ν120.3
Yield stress (Mpa)[ 30, 33, 37 ]
Plastic strain[ 0, 0.02, 0.05 ]
Table 2

Value ranges before and after normalization

Channel/DataOriginal rangeNormalized range
Input Channel 1 (Cell Types){0, 1, 2, 3, 4, 5}[0,1]
Input Channel 2 (Feature Matrices){30, 1700, 135,000}[0,1]
Output Data (Re and Rν, Ratios)[0,2][0,1]
Table 3

Training and performance hyperparameters for benchmark CNN models

ParameterResNet-18Deep Baseline CNN
Input size2 × 500 × 5002 × 500 × 500
Parameter quantity12.5 m11m
Batch size6464
Learning rate1 × 10–31 × 10–3
OptimizerAdamAdam
Weight decay1 × 10–51 × 10–5
Data augmentationRandom flips, cropsRandom flips, crops
Epochs100110
Training time (wall-clock)6 h6.5 h
GPU memory peak8 GB8 GB
Inference latency per sample45 ms50 ms
List of channels in conv layers[ 64, 128, 256, 512 ][ 64, 128, 256, 512 ]
Sizes of FC hidden layers[ 512, 1,024, 256 ][ 512, 1,024, 256 ]
Dropout rate0.30.3
Table 4

Tunable hyperparameters in the CNN architecture and training pipeline

ParameterDescriptionDefault value
block_chNumber of filters in block pooling layer256
block_sizeSize/stride of block pooling kernel100
conv_chsList of channels in conv layers[256, 128, 64, 32, 16, 8]
fc_dimsSizes of FC hidden layers[512, 256, 64]
dropout_rateDropout probability in FC layers0.4
learning_rateLearning rate for Adam optimizer1 × 10–3
batch_sizeNumber of samples per batch128
num_epochsTotal number of training epochs120
val_splitValidation set fraction0.15
test_splitTest set fraction0.15
output_dimDimension of output (Re, Rν)2
in_channelsInput channels (geometry and features)2
Table 5

Training and inference resource metrics for CNN models

ModelEpoch timeConverging epochGPU memInference
Model-1180s1008 GB55 ms
Model-2115s1108 GB61 ms
Lightweight model35s806 GB3.5 ms
Table 6

Training and inference resource metrics for benchmark models

ModelTime/structureTime cost totalCost reduction
FF simulation33 ± 1.3 min16,500 min/
Homogenized simulation2.35 ± 0.15 min1,175 min93.81%
Model-1 informed5.85 ± 0.27 min2,925 min82.27%
Model-2 informed5.99 ± 0.31 min2,995 min81.84%
Lightweight model2.5 ± 0.12 min1,250 min92.42%

Supplements

References

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