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A New Method to Predict Damage to Composite Structures Using Convolutional Neural Networks
Laurent Mezeix1, Ainhoa Soldevila Rivas2, Antonin Relandeau2
1Faculty of Engineering, Burapha University, 169 Long-Hard Bangsaen Road, Chonburi 20131, Thailand.
Materials (Basel, Switzerland)
|November 25, 2023
Summary
Artificial intelligence, specifically deep learning, can predict impact damage in fiber-reinforced polymer (FRP) composites. An aggregated convolutional neural network (CNN) model shows significant potential for accelerating composite design with high precision.
Area of Science:
- Materials Science
- Mechanical Engineering
- Computational Science
Background:
- Virtual testing and finite element methods (FEMs) are crucial for predicting damage in composite aeronautical structures.
- FEMs for composite impact analysis are computationally intensive and require significant expertise.
- Artificial intelligence offers a promising alternative for efficient composite damage assessment.
Purpose of the Study:
- To develop and evaluate a deep learning methodology for predicting impact damage in fiber-reinforced polymer (FRP) composites.
- To explore the effectiveness of convolutional neural network (CNN) architectures for this prediction task.
- To demonstrate the potential of AI in accelerating the design process for composite structures.
Main Methods:
- A deep learning approach utilizing CNN models was developed.
- Data was sourced from literature and FEM simulations, augmented to increase dataset size from 149 to 2725 instances.
- Two CNN architectures were aggregated and compared against a single CNN model.
Main Results:
- The aggregated CNN model outperformed a single CNN architecture.
- The model achieved a precision of 0.15 mm for length measurements.
- Average delaminated surface error was 56 mm², with a 7% error rate for delamination presence prediction.
Conclusions:
- Aggregated CNN models show strong potential for accurately predicting impact damage in composites.
- This AI-driven approach can significantly accelerate the design cycle for aeronautical composite structures.
- The methodology offers a more efficient alternative to traditional FEM-based virtual testing.

