A model for thermal protection ablative material with local thermal non-equilibrium and thermal radiation mechanisms-Reference-Cited by-同舟云学术

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A model for thermal protection ablative material with local thermal non-equilibrium and thermal radiation mechanisms

Published:2021-06 Issue: Volume:183 Page:101-111
ISSN:0094-5765
Container-title:Acta Astronautica
language:en
Short-container-title:Acta Astronautica

Author:

Li Weijie,Huang Jie,Zhang Zhongwei,Wang Liyan,Huang Haiming,Liang Jun

Funder

National Natural Science Foundation of China

Fundamental Research Funds for the Central Universities

Publisher

Elsevier BV

Subject

Aerospace Engineering

Reference27 articles.

1. Experimental study on erosion characteristics of char layer of EPDM composite by cold flow;Li;Acta Astronaut.,2019

2. Novel phenolic impregnated 3-D Fine-woven pierced carbon fabric composites: microstructure and ablation behavior;Hong;Compos. B Eng.,2012

3. Mathematical model for analyzing heat transfer characteristics of ablative thermal insulating material;Gao;Int. J. Aerospace Eng.,2020

4. Manufacturing, thermochemical characterization and ablative performance evaluation of carbon-phenolic ablative material with nano-Al2O3 addition;Paglia;Polym. Degrad. Stabil.,2019

5. Advances in ablative composites of carbon based materials: a review;Kumar;Ind. Eng. Chem. Res.,2019

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4. High-temperature broadband infrared radiation from rare earth monosilicate-based ceramics;Journal of the European Ceramic Society;2024-09

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