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Hai-Ming HUANG Wei-Jie LI Hai-Ling YU


Charring thermal protection systems have been used to protect hypersonic vehicles from high heat loads. The pyrolysis of charring materials is a complicated physical and chemical phenomenon. Based on the pyrolysis interface model, a simulating approach for charring ablation has been designed in order  to obtain one dimensional transient thermal behavior of homogeneous charring materials in reentry capsules. As the numerical results indicate, the pyrolysis rate and the surface temperature under a given heat flux rise abruptly in the beginning, then reach a plateau, but the temperature at the bottom rises very slowly to prevent the structural materials from being heated seriously. Pyrolysis mechanism can play an important role in thermal protection systems subjected to serious aerodynamic heat.

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HUANG, Hai-Ming; LI, Wei-Jie; YU, Hai-Ling. THERMAL ANALYSIS OF CHARRING MATERIALS BASED ON PYROLYSIS INTERFACE MODEL. Thermal Science, [S.l.], v. 18, n. 5, p. 1591-1596, jan. 2017. ISSN 2334-7163. Available at: <>. Date accessed: 17 oct. 2017. doi:
Received 2017-01-24
Accepted 2017-01-25
Published 2017-01-25


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