One-Dimensional Thermal Analysis Model for Charring Ablative Materials
This paper presents a one-dimensional model for the analysis of the charring ablative materials used in spacecraft thermal protection systems. The numerical method is based on an implicit finite difference formulation of the governing equations written for a system of mobile coordinates that accoun...
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| Format: | Article |
| Language: | English |
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Instituto de Aeronáutica e Espaço (IAE)
2018-02-01
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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/965 |