Superior ablation resistance of C/C-HfC-SiC composite sharp leading edges above 2500 °C prepared by precursor infiltration and pyrolysis-Reference-Cited by-同舟云学术

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Superior ablation resistance of C/C-HfC-SiC composite sharp leading edges above 2500 °C prepared by precursor infiltration and pyrolysis

Published:2024-05 Issue: Volume: Page:
ISSN:2352-8478
Container-title:Journal of Materiomics
language:en
Short-container-title:Journal of Materiomics

Author:

Li Wei,Lv Junshuai,Li Jingtong,Guo Lingxiang,Zhang Yutai,Shi Xiaohong,Li Hejun

Publisher

Elsevier BV

Reference56 articles.

1. ZrB2-SiC sharp leading edges in high enthalpy supersonic flows;Monteverde;J Am Ceram Soc,2012

2. Thermal and oxidation response of UHTC leading edge samples exposed to simulated hypersonic flight conditions;Parthasarathy;J Am Ceram Soc,2013

3. Material property requirements for analysis and design of UHTC components in hypersonic applications;Squire;J Eur Ceram Soc,2010

4. Constructing orthogonally structured graphene nanointerface on SiC nanowires reinforced carbon/carbon composites to boost mechanical strength and strength retention rate;Guo;J Materiomics,2024

5. Advanced structural ceramics in aerospace propulsion;Padture;Nat Mater,2016

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