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E/TBCs advanced material systems can revolutionize the aerospace and related industries by providing means to build fuel-efficient turbine engines operating at elevated temperatures.
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A 3D peridynamic model to account for heat transfer was implemented in MesoEqs
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Demonstration was performed for heat transfer in a quasi-2D domain
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Peridynamic results were compared with an analytical solution
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This peridynamic heat model can be used for modeling transient heat conduction in material structures with evolving discontinuities


