SIMULATION OF ABLATION IN A COMPOSITE THERMAL PROTECTION SYSTEM VIA AN INTERFACE TRACKING METHOD DOI 10.5028/jatm.2012.04030312
In this work, the two-dimensional computational simulation of the ablative process in a composite used in rocket thermal protection systems via an interface tracking method was presented. The ablative model considers the presence of two simultaneous moving fronts, the pyrolysis and char fronts. The...
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| Format: | Article |
| Language: | English |
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Instituto de Aeronáutica e Espaço (IAE)
2012-10-01
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| Series: | Journal of Aerospace Technology and Management |
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| Online Access: | https://www.jatm.com.br/jatm/article/view/174 |