​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.

A 3D peridynamic model to account for heat transfer was implemented in MesoEqs

Demonstration was performed for heat transfer in a quasi-2D domain 

Peridynamic results were compared with an analytical solution

This peridynamic heat model can be used for modeling transient heat conduction in material structures with evolving discontinuities