Space-time asymptotic expansion method (AEM) is a rigorous method for solving the multiscale transient thermal conduction problem in periodic composites. However, the AEM is still difficult to model the thermal behavior in composites when temperature-dependent material properties are taken into account. Besides, its complex and costly implementation also restricts the usage of AEM. A space–time AEM for multiscale transient thermal analysis is comprehensively studied in this study to address these issues properly. After the constitutive equation of temperature-dependent characteristic temperature tensor and effective thermal properties in the transient thermal conduction is deduced from the solid theoretical base, a new implementation approach comprised of both homogenization and localization is developed. It can directly model the characteristic temperature tensor within a representative volume element model under simple periodic boundary conditions and linear temperature loads, differing from conventional AEM, which requires complex location-related heat flux loads. Moreover, a new characteristic heat flux tensor is proposed to replace the characteristic temperature tensor in the localization of heat flux. All these contributions simplify the localization in the new implementation. The thermal behavior of A fiber-reinforced composite during the forming process is investigated using the space–time AEM and multiscale finite element method. The comparison results between space–time AEM and multiscale finite element method indicate that the space–time AEM is accurate and efficient as the differences of local temperature and heat flux are 0.0051 °C and 7.2 × 10-5 W/mm2, and the total nodes in space–time AEM is only about half of the multiscale finite element method.
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