Carbon fiber reinforced silicon carbide composite-based sharp leading edges in high enthalpy plasma flows
Authors:
- Lei LuoLLLei Luo
- Yiguang WangYWYiguang Wang
- Liping LiuLLLiping Liu
- Xing ZhaoXZXing Zhao
- Yonghong LuYLYonghong Lu
- Guolin WangGWGuolin Wang
- 1 February 2018
- journal article
- research article
- Published by Elsevier in Composites Part B: Engineering
- Vol. 135, 35-42
Abstract
No abstract availableKeywords
Funding Information
- National Natural Science Foundation of China (51172181, 51521061)
- 111 (B08040)
This publication has 48 references indexed in Scilit:
- Ablation behavior of C/SiC composites in plasma wind tunnelCarbon, 2016
- Development of multi-layered thermal protection system (TPS) for aerospace applicationsComposites Part B: Engineering, 2015
- Ablation behavior and mechanism of SiC/Zr–Si–C multilayer coating for PIP-C/SiC composites under oxyacetylene torch flameComposites Part B: Engineering, 2015
- Surface temperature jump beyond active oxidation of carbon/silicon carbide composites in extreme aerothermal conditionsCarbon, 2014
- Design, preparation and properties of online-joints of C/SiC–C/SiC with pinsComposites Part B: Engineering, 2013
- ZrB2/SiC as a protective coating for C/SiC composites: Effect of high temperature oxidation on mechanical properties and anti-ablation propertyComposites Part B: Engineering, 2013
- Effects of low earth orbit environments on atomic oxygen undercutting of spacecraft polymer filmsComposites Part B: Engineering, 2013
- C/SiC–ZrB2–ZrC composites fabricated by reactive melt infiltration with ZrSi2 alloyCeramics International, 2012
- C/C–SiC–ZrC composites fabricated by reactive melt infiltration with Si0.87Zr0.13 alloyCeramics International, 2012
- Atomic oxygen resistant coatings for low earth orbit space structuresJournal of Materials Science, 1995