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International Journal of Aerospace Engineering
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International Journal of Aerospace Engineering
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2017
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Article
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Tab 10
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Research Article
Performance of Gradient-Based Solutions versus Genetic Algorithms in the Correlation of Thermal Mathematical Models of Spacecrafts
Table 10
Heat flows (W).
Parameter
Case 1
41.24
24.53
54.22
ā4.267
45.51
20.27
Case 2
30.93
28.62
60.44
ā8.53
39.47
20.09