Carbon fiber reinforced silicon carbide composite-based sharp leading edges in high enthalpy plasma flows

Lei Luo; Yiguang Wang; Liping Liu; Xing Zhao; Yonghong Lu; Guolin Wang

doi:10.1016/j.compositesb.2017.09.060

Carbon fiber reinforced silicon carbide composite-based sharp leading edges in high enthalpy plasma flows

Lei Luo, Yiguang Wang^*, Liping Liu, Xing Zhao, Yonghong Lu, Guolin Wang

^*Corresponding author for this work

Research output: Contribution to journal › Article › peer-review

39 Citations (Scopus)

Abstract

Carbon fiber-reinforced silicon carbide (C/SiC) and zirconium diboride-zirconium carbide (ZrB₂-ZrC) modified C/SiC (C/SiC-ZrB₂-ZrC) sharp leading edges (SLEs) were prepared in this study. Their ablation behaviors were tested in plasma wind tunnels. The results indicated that the ablation of C/SiC SLEs was controlled by the atomic oxidation of SiC, leading to the elimination of SiC. In contrast, C/SiC-ZrB₂-ZrC SLEs showed little reduction in plasma flows. During ablation, a ZrO₂ skeleton was formed with silica filling inside by the atomic oxidation of SiC. The ZrO₂ skeleton suppressed the consumption of SiC, resulting in the improvement of the ablation resistance of C/SiC-ZrB₂-ZrC SLEs.

Original language	English
Pages (from-to)	35-42
Number of pages	8
Journal	Composites Part B: Engineering
Volume	135
DOIs	https://doi.org/10.1016/j.compositesb.2017.09.060
Publication status	Published - 15 Feb 2018
Externally published	Yes

Keywords

Ceramic-matrix composites (CMCs)
Corrosion
Electron microscopy
High-temperature properties

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10.1016/j.compositesb.2017.09.060

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@article{4dbdb0f1d02b4c8fa895fda0f7773a51,

title = "Carbon fiber reinforced silicon carbide composite-based sharp leading edges in high enthalpy plasma flows",

abstract = "Carbon fiber-reinforced silicon carbide (C/SiC) and zirconium diboride-zirconium carbide (ZrB2-ZrC) modified C/SiC (C/SiC-ZrB2-ZrC) sharp leading edges (SLEs) were prepared in this study. Their ablation behaviors were tested in plasma wind tunnels. The results indicated that the ablation of C/SiC SLEs was controlled by the atomic oxidation of SiC, leading to the elimination of SiC. In contrast, C/SiC-ZrB2-ZrC SLEs showed little reduction in plasma flows. During ablation, a ZrO2 skeleton was formed with silica filling inside by the atomic oxidation of SiC. The ZrO2 skeleton suppressed the consumption of SiC, resulting in the improvement of the ablation resistance of C/SiC-ZrB2-ZrC SLEs.",

keywords = "Ceramic-matrix composites (CMCs), Corrosion, Electron microscopy, High-temperature properties",

author = "Lei Luo and Yiguang Wang and Liping Liu and Xing Zhao and Yonghong Lu and Guolin Wang",

note = "Publisher Copyright: {\textcopyright} 2017 Elsevier Ltd",

year = "2018",

month = feb,

day = "15",

doi = "10.1016/j.compositesb.2017.09.060",

language = "English",

volume = "135",

pages = "35--42",

journal = "Composites Part B: Engineering",

issn = "1359-8368",

publisher = "Elsevier Ltd.",

}

TY - JOUR

T1 - Carbon fiber reinforced silicon carbide composite-based sharp leading edges in high enthalpy plasma flows

AU - Luo, Lei

AU - Wang, Yiguang

AU - Liu, Liping

AU - Zhao, Xing

AU - Lu, Yonghong

AU - Wang, Guolin

PY - 2018/2/15

Y1 - 2018/2/15

N2 - Carbon fiber-reinforced silicon carbide (C/SiC) and zirconium diboride-zirconium carbide (ZrB2-ZrC) modified C/SiC (C/SiC-ZrB2-ZrC) sharp leading edges (SLEs) were prepared in this study. Their ablation behaviors were tested in plasma wind tunnels. The results indicated that the ablation of C/SiC SLEs was controlled by the atomic oxidation of SiC, leading to the elimination of SiC. In contrast, C/SiC-ZrB2-ZrC SLEs showed little reduction in plasma flows. During ablation, a ZrO2 skeleton was formed with silica filling inside by the atomic oxidation of SiC. The ZrO2 skeleton suppressed the consumption of SiC, resulting in the improvement of the ablation resistance of C/SiC-ZrB2-ZrC SLEs.

AB - Carbon fiber-reinforced silicon carbide (C/SiC) and zirconium diboride-zirconium carbide (ZrB2-ZrC) modified C/SiC (C/SiC-ZrB2-ZrC) sharp leading edges (SLEs) were prepared in this study. Their ablation behaviors were tested in plasma wind tunnels. The results indicated that the ablation of C/SiC SLEs was controlled by the atomic oxidation of SiC, leading to the elimination of SiC. In contrast, C/SiC-ZrB2-ZrC SLEs showed little reduction in plasma flows. During ablation, a ZrO2 skeleton was formed with silica filling inside by the atomic oxidation of SiC. The ZrO2 skeleton suppressed the consumption of SiC, resulting in the improvement of the ablation resistance of C/SiC-ZrB2-ZrC SLEs.

KW - Ceramic-matrix composites (CMCs)

KW - Corrosion

KW - Electron microscopy

KW - High-temperature properties

UR - http://www.scopus.com/inward/record.url?scp=85030863793&partnerID=8YFLogxK

U2 - 10.1016/j.compositesb.2017.09.060

DO - 10.1016/j.compositesb.2017.09.060

M3 - Article

AN - SCOPUS:85030863793

SN - 1359-8368

VL - 135

SP - 35

EP - 42

JO - Composites Part B: Engineering

JF - Composites Part B: Engineering

ER -

Carbon fiber reinforced silicon carbide composite-based sharp leading edges in high enthalpy plasma flows

Abstract

Keywords

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