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

<table class="table-group" id="tab5"><tr><td><table class="table"><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr class="thead"><td class="align_left">Material type</td><td class="align_center">A</td><td class="align_center">B</td><td class="align_center">C</td></tr><tr><td class="thead-hr" colspan="4"><hr/></td></tr><tr><td class="align_left">Deviation (%)</td><td class="align_center">17.02</td><td class="align_center">13.62</td><td class="align_center">12.18</td></tr><tr class="table-tr"><td colspan="4"><hr class="tbody-hr"/></td></tr></table></td></tr></table>

<div>Comparison between the crosslinked model and experimental result.</div>

International Journal of Aerospace Engineering

tab5

Table 5

Table 5: Prediction of Heat Transfer Characteristics of the Carbonized Layer of Resin-Based Ablative Material Based on the Finite Element Method 