High-temperature transient-induced thermomechanical damage of fiber-reinforced ceramic-matrix composites in supersonic wind tunnel
文献类型：期刊论文
| 作者 | Wang JT(王江涛)3 ; Yang ZM(杨正茂)2; Yang, Rui1; Jiao, Jian1; Yue LJ(岳连捷)2; Hou, Xiao3
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| 刊名 | COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING
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| 出版日期 | 2024-09-01 |
| 卷号 | 184页码:11 |
| 关键词 | 1.050: Ceramic-matrixcomposites (CMCs) 2.160: Environmental degradation 4.160: Failure 5.210: Lay-up(mannual/automate) 6:Transient thermal gradients |
| ISSN号 | 1359-835X |
| DOI | 10.1016/j.compositesa.2024.108243 |
| 通讯作者 | Yang, Zhengmao(zmyang@imech.ac.cn) |
| 英文摘要 | This article is based on the supersonic directly connected wind tunnel. Through a specially designed experimental chamber, combined with infrared temperature measurement, high-speed camera, etc., in -situ monitoring of composite materials under airflow at Ma 3.0 with a total temperature of 950 similar to 1473K was carried out. The dimensional analysis method was used to propose dimensionless parameters to characterize the thermal coupling caused by high-speed airflow thermal shock. Research has shown that the thermal coupling effect of supersonic airflow causes uneven temperature inside the material, and the thermal stress caused by temperature gradient changes (including increasing and decreasing processes) is the main reason for material damage. The damage of ceramic matrix composites under thermal shock mainly manifests as a decrease in surface roughness, surface fiber fracture and a decrease in elastic modulus. In addition, the study also found that there are damage thresholds for the thermal shock effect of airflow at different total temperatures, which helps to further understand the thermomechanical damage mechanism and degradation law of composite structure under high -temperature transient conditions. |
| 分类号 | 一类 |
| WOS关键词 | MECHANICAL-BEHAVIOR |
| WOS研究方向 | Engineering ; Materials Science |
| 语种 | 英语 |
| WOS记录号 | WOS:001263007100001 |
| 其他责任者 | Yang, Zhengmao |
| 源URL | [http://dspace.imech.ac.cn/handle/311007/95956]  |
| 专题 | 宽域飞行工程科学与应用中心 力学研究所_高温气体动力学国家重点实验室 |
| 作者单位 | 1.AECC Beijing Inst Aeronaut Mat, Natl Key Lab Adv Composites, Beijing 100095, Peoples R China 2.Chinese Acad Sci, Inst Mech, Beijing 100190, Peoples R China; 3.Beijing Inst Technol, Sch Aerosp Engn, Beijing 100081, Peoples R China; |
| 推荐引用方式 GB/T 7714 | Wang JT,Yang ZM,Yang, Rui,et al. High-temperature transient-induced thermomechanical damage of fiber-reinforced ceramic-matrix composites in supersonic wind tunnel[J]. COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING,2024,184:11. |
| APA | 王江涛,杨正茂,Yang, Rui,Jiao, Jian,岳连捷,&Hou, Xiao.(2024).High-temperature transient-induced thermomechanical damage of fiber-reinforced ceramic-matrix composites in supersonic wind tunnel.COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING,184,11. |
| MLA | 王江涛,et al."High-temperature transient-induced thermomechanical damage of fiber-reinforced ceramic-matrix composites in supersonic wind tunnel".COMPOSITES PART A-APPLIED SCIENCE AND MANUFACTURING 184(2024):11. |
入库方式： OAI收割
来源：力学研究所
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