This paper presents a multifield numerical approach to analyze the thermochemical behavior of composite structures during curing. A 1D high-fidelity model, developed within the Carrera Unified Formulation (CUF) and the Finite Element Method (FEM), is employed to solve the coupled heat-transfer and cure-kinetics equations. This approach allows accurate prediction of both temperature and degree of cure during the curing cycle, providing full 3D distributions for these variables. The modeling approach is layer-wise (LW), with each ply explicitly modeled and having a set of unknown variables. The proposed methodology is applied to graphite/epoxy composite laminates and extended to a hybrid solid laminate/honeycomb structure, demonstrating its applicability to both monolithic and complex structures. The influence of different boundary conditions, such as temperature and free-surface convection, and non-homogeneous convection, is analyzed. The results consider the time evolution of temperature and degree of cure, and the 3D distribution within the composite part. The model’s accuracy is verified through results from the literature.
Temperature and degree of cure 3D distributions in fiber-reinforced and sandwich composites using 1D finite elements / Zappino, E.; Santori, M.; Zobeiry, N.; Petrolo, M.. - In: MECHANICS OF MATERIALS. - ISSN 0167-6636. - ELETTRONICO. - 217:(2026). [10.1016/j.mechmat.2026.105651]
Temperature and degree of cure 3D distributions in fiber-reinforced and sandwich composites using 1D finite elements
Zappino, E.;Santori, M.;Zobeiry, N.;Petrolo, M.
2026
Abstract
This paper presents a multifield numerical approach to analyze the thermochemical behavior of composite structures during curing. A 1D high-fidelity model, developed within the Carrera Unified Formulation (CUF) and the Finite Element Method (FEM), is employed to solve the coupled heat-transfer and cure-kinetics equations. This approach allows accurate prediction of both temperature and degree of cure during the curing cycle, providing full 3D distributions for these variables. The modeling approach is layer-wise (LW), with each ply explicitly modeled and having a set of unknown variables. The proposed methodology is applied to graphite/epoxy composite laminates and extended to a hybrid solid laminate/honeycomb structure, demonstrating its applicability to both monolithic and complex structures. The influence of different boundary conditions, such as temperature and free-surface convection, and non-homogeneous convection, is analyzed. The results consider the time evolution of temperature and degree of cure, and the 3D distribution within the composite part. The model’s accuracy is verified through results from the literature.| File | Dimensione | Formato | |
|---|---|---|---|
|
ZSZP_MECHMAT_2026.pdf
accesso riservato
Tipologia:
2a Post-print versione editoriale / Version of Record
Licenza:
Non Pubblico - Accesso privato/ristretto
Dimensione
2.6 MB
Formato
Adobe PDF
|
2.6 MB | Adobe PDF | Visualizza/Apri Richiedi una copia |
|
ZSZP_MECHMAT_2025_Revised.pdf
embargo fino al 05/03/2028
Tipologia:
2. Post-print / Author's Accepted Manuscript
Licenza:
Creative commons
Dimensione
1.63 MB
Formato
Adobe PDF
|
1.63 MB | Adobe PDF | Visualizza/Apri Richiedi una copia |
Pubblicazioni consigliate
I documenti in IRIS sono protetti da copyright e tutti i diritti sono riservati, salvo diversa indicazione.
https://hdl.handle.net/11583/3008435
