Moving boundary problem of ablation in a carbon-phenolic composite using finite element method
Author:
Publisher
Springer Science and Business Media LLC
Subject
Mechanical Engineering,General Engineering,Aerospace Engineering,Automotive Engineering,Industrial and Manufacturing Engineering,Applied Mathematics
Link
https://link.springer.com/content/pdf/10.1007/s40430-021-03230-y.pdf
Reference49 articles.
1. Khan MB (1996) An investigation of the ablation behavior of advanced ultrahigh-temperature epdm/epoxy insulation composites. Polym-Plast Technol Eng 35(1):187–206. https://doi.org/10.1080/03602559608000088
2. Wang Z, Chen SYu (2015) Ablation behavior and mechanism analysis of C/SiC composites. J Mater Res Technol 5:170–182. https://doi.org/10.1016/j.jmrt.2015.10.004
3. Kumar S (2015) Fabrication and ablation studies of 4d c/sic composite nozzle under liquid propulsion. Int J Appl Ceram Technol. https://doi.org/10.1111/ijac.12392
4. Pacheeri S, Kandasubramanian B (2014) Hybrid carbon-carbon ablative composites for thermal protection in aerospace. j Compos. https://doi.org/10.1155/2014/825607
5. Ruperti Jr., NJ (1991) Solution of a one-dimensional ablation model. M.Sc. Thesis. INPE. Brazil. (in Portuguese).
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