Structures requiring robust maintenance and accessibility pose challenges for structural integrity monitoring. This monitoring, crucial in various engineering applications, enables corrective actions to ensure machinery and equipment safety. Laminated composite materials, prevalent in aeronautical structures, often exhibit imperceptible delaminations or cracks, demanding the use of artificial intelligence for damage characterization. This study employs a numerical-experimental methodology, integrating artificial neural networks, to identify delaminations. Delamination, a structural damage form, was intentionally induced in epoxy-fiberglass composite structures. Modal tests captured characteristics in damaged and undamaged structures, revealing artificial intelligence effectiveness in pinpointing damage location and size. Damage significantly altered beam mode shapes, generating complex modes. Induced delaminations led to a measurable 15% reduction in natural frequencies, and damping ratios increased by approximately 10% in damaged structures. Artificial neural networks achieved an impressive 92% accuracy in predicting delamination location and size. Quantitative analysis of mode shape alterations validated the proposed methodology's efficacy. This study provides valuable quantitative insights into damage detection in laminated composite structures, highlighting AI's potential for enhanced structural health monitoring. The numerical-experimental approach, supported by quantitative results, emphasizes the importance of advanced techniques for precise and efficient damage characterization in critical engineering applications. HIGHLIGHTS The study presents a significant advancement in delamination detection in composite structures using deep learning, offering an innovative approach to structural integrity monitoring. The article effectively combines numerical and experimental data, showcasing the successful application of finite element models and modal tests to enhance damage detection accuracy. The research employs detailed modeling of delamination, including variations in size, location, and affected layers, enabling precise identification of damage extent and severity. Artificial neural networks (ANNs) are effectively employed to predict delamination location and size, highlighting the potential of ANNs in structural monitoring applications The obtained results hold significant implications for the safety of composite structures, particularly in aerospace applications where early damage detection is crucial to prevent catastrophic failures