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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
/
2019
/
Article
/
Tab 6
/
Research Article
Prediction of Heat Transfer Characteristics of the Carbonized Layer of Resin-Based Ablative Material Based on the Finite Element Method
Table 6
Comparison between random model and experimental result.
Model type
Thermal conductivity coefficient (W·m
-1
·K
-1
)
A
B
C
Random model
0.4422
0.4633
0.4990
Experiment result
0.45
0.423
0.5
Deviation (%)
1.74
9.53
0.192