Aerospace Science and Technology, Год журнала: 2025, Номер unknown, С. 110363 - 110363
Опубликована: Июнь 1, 2025
Язык: Английский
Aerospace Science and Technology, Год журнала: 2025, Номер unknown, С. 110363 - 110363
Опубликована: Июнь 1, 2025
Язык: Английский
IEEE Access, Год журнала: 2025, Номер 13, С. 10252 - 10264
Опубликована: Янв. 1, 2025
Язык: Английский
Процитировано
1International Journal of Mechanical Sciences, Год журнала: 2025, Номер unknown, С. 110137 - 110137
Опубликована: Март 1, 2025
Язык: Английский
Процитировано
1Mathematics, Год журнала: 2024, Номер 13(1), С. 17 - 17
Опубликована: Дек. 25, 2024
Physics-Informed Neural Networks (PINNs) integrate physics principles with machine learning, offering innovative solutions for complex modeling challenges. Laminated composites, characterized by their anisotropic behavior, multi-layered structures, and intricate interlayer interactions, pose significant challenges traditional computational methods. PINNs address these issues embedding governing physical laws directly into neural network architectures, enabling efficient accurate modeling. This review provides a comprehensive overview of applied to laminated highlighting advanced methodologies such as hybrid PINNs, k-space Theory-Constrained optimal disjointed PINNs. Key applications, including structural health monitoring (SHM), analysis, stress-strain failure multi-scale modeling, are explored illustrate how optimize material configurations enhance reliability. Additionally, this examines the associated deploying identifies future directions further advance capabilities. By bridging gap between classical physics-based models data-driven techniques, advances understanding PINN composites underscores transformative role in addressing complexities solving real-world problems.
Язык: Английский
Процитировано
7Thin-Walled Structures, Год журнала: 2025, Номер unknown, С. 112970 - 112970
Опубликована: Янв. 1, 2025
Язык: Английский
Процитировано
0International Communications in Heat and Mass Transfer, Год журнала: 2025, Номер 164, С. 108954 - 108954
Опубликована: Апрель 11, 2025
Язык: Английский
Процитировано
0Journal of Sandwich Structures & Materials, Год журнала: 2025, Номер unknown
Опубликована: Апрель 19, 2025
Sandwich structures with composite laminate panels have gained increasing prominence in the aerospace, automotive, and transportation industries, particularly design of high-performance components such as aircraft fuselages, automotive bodies, infrastructure. Their exceptional specific strength, stiffness, improved structural stability make them critical these industries for enhancing performance while reducing weight. However, accurately predicting their buckling behavior under compressive loads remains a significant challenge, traditional isotropic plate models are often inadequate. To address this issue, study develops an innovative theoretical model sandwich panels, integrating stress function method first-order shear deformation theory (FSDT) to capture unique characteristics laminated composites. The produces exact closed-form solutions global wrinkling, offering valuable insights into underlying mechanisms. A sufficiently broad range material parameter ratios, including face-to-core stiffness ratio, thickness aspect were selected based on realistic engineering conditions. analytical solution was rigorously validated against three-dimensional finite element (FEM) structure orthotropic face sheets, demonstrating high agreement FEM simulations, maximum deviation less than 6%. This proposed approach provides rapid effective means verifying numerical simulation accuracy, establishing robust foundation optimization structures.
Язык: Английский
Процитировано
0Composite Structures, Год журнала: 2025, Номер unknown, С. 119264 - 119264
Опубликована: Май 1, 2025
Язык: Английский
Процитировано
0Energy, Год журнала: 2025, Номер unknown, С. 136862 - 136862
Опубликована: Май 1, 2025
Язык: Английский
Процитировано
0Aerospace Science and Technology, Год журнала: 2025, Номер unknown, С. 110363 - 110363
Опубликована: Июнь 1, 2025
Язык: Английский
Процитировано
0