The invention discloses a resin-based material
ablation heat transfer simulation method considering
microstructure evolution, which comprises the following steps of:
cutting material samples from different positions of a pneumatically heated material to obtain a
material density value, calculating to obtain a
pyrolysis degree, further obtaining matrix physical properties under different
pyrolysis degrees, and simultaneously observing the
microstructure of each material sample to obtain the
thermal conductivity of the resin-based material. According to the method, the
microstructure morphology, the
lap joint relation between microstructure components and the
mutual position relation are obtained, the evolution law of the microstructure in the
aerodynamic heating process is obtained according to the statistical result, the morphology observation result of the microstructure is combined, a finite
element model is established, and boundary conditions are loaded for solving. And carrying out fitting on the equivalent heat
conductivity relationships corresponding to the different
pyrolysis degrees to obtain a fitting relational expression of the heat
conductivity of the resin-based material along with the change of the pyrolysis degrees so as to replace a corrected linear interpolation relational expression in the
ablation heat transfer calculation model of the resin-based material, and calculating the
ablation heat transfer of the resin-based material according to the fitting relational expression. Therefore, the ablation
heat transfer model of the resin-based material is improved.