Prediction of Heat Transfer Characteristics of the Carbonized Layer of Resin-Based Ablative Material Based on the Finite Element Method

<div>Carbon deposited image of the resin matrix ablation material’s carbonized layer: (a) 300 times magnified image and (b) 100 times magnified image.</div>

International Journal of Aerospace Engineering

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Figure 12

Figure 12: Prediction of Heat Transfer Characteristics of the Carbonized Layer of Resin-Based Ablative Material Based on the Finite Element Method 