Thermomechanical modeling of dissimilar-material interfaces in composite structures

• Published in: International journal of mechanical sciences Vol. 266; p. 108919
• Main Authors: Ahmed, S Reaz, Nath, Methu Dev, Amin, M Farhan, Datta, Bibekananda
• Format: Journal Article
• Language: English
• Published: Elsevier Ltd 15-03-2024
• Subjects: Displacement-function; Dissimilar-material interface; Fiber-reinforced composites; Stress singularity; Structural mechanics; Thermoelasticity; Fiber-reinforced composites; Stress singularity; Thermoelasticity; Dissimilar-material interface; Structural mechanics; Displacement-function
• ISSN: 0020-7403; 1879-2162
• DOI: 10.1016/j.ijmecsci.2023.108919

•An alternative model for thermomechanical interfaces in multi-material composites•Displacement-function based semi-analytical solution for thermo-mechanical stresses•Alternative computational stencils are designed for the interfaces and interface corners•Prediction of stress singularity at free interface corners is highly localized compared to FEM•Equally effective scheme for problems with uniform and mixed-mode physical conditions
Due to the heterogeneities in material properties of strongly-bonded multi-material composite structures, there exist singularities of the stress fields at the material interface as well as the interface corners on the bounding surfaces. The finite-element method is probably the only plausible option to analyze the stress around such interfaces between dissimilar materials subjected to combined thermo-mechanical loading. In this article, we propose a novel mathematical model for the computational analysis of coupled thermo-elastic fields with perfectly bonded interfaces of dissimilar isotropic/orthotropic composite-material structures. A scalar function of the spatial variables, namely, the displacement function, is used to integrate the temperature field and the associated displacement-function field to obtain two nonhomogeneous partial-differential equations of equilibrium that govern two thermo-mechanical sub-problems defined in terms of the appropriate conditions of orthogonal temperature gradients. For a specific temperature field, obtained as a steady-state solution of the given thermal problem, the two thermo-mechanical sub-problems are solved independently to obtain the full-field solution of the thermo-elastic problem using the method of superposition. As an alternative to the conventional computational approach, we employed a single variable semi-analytical method of solution to determine the thermo-mechanical response of the multi-material composite structures. The continuity of the temperature and the heat flux in the thermal field problem and the continuity of the displacement and the traction vectors are utilized in the elastic field problem to determine the appropriate algebraic equations suitable for nodal application at the interfaces as well as interface corners on the boundaries of the respective problems. The quantitative comparison of the present displacement-function solutions to several mixed-boundary-value problems with those obtained by the conventional finite-element method verifies the high accuracy and effectiveness of the present method. This computational model has potential applications in identifying near-interface high-stress locations as well as possible critical regions of the physical boundary of composite structures subjected to mixed modes of thermal and mechanical loadings.
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