High-temperature transient-induced thermomechanical damage of fiber-reinforced ceramic-matrix composites in supersonic wind tunnel-Reference-Cited by-同舟云学术

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High-temperature transient-induced thermomechanical damage of fiber-reinforced ceramic-matrix composites in supersonic wind tunnel

Published:2024-09 Issue: Volume:184 Page:108243
ISSN:1359-835X
Container-title:Composites Part A: Applied Science and Manufacturing
language:en
Short-container-title:Composites Part A: Applied Science and Manufacturing

Author:

Wang Jiangtao,Yang Zhengmao,Yang Rui,Jiao Jian,Yue Lianjie,Hou Xiao

Funder

National Natural Science Foundation of China

Publisher

Elsevier BV

Reference32 articles.

1. Interlaminar response of LSI-produced C/SiC ceramic matrix composites: Experiments and modelling;Riva;Compos A,2023

2. Coating recession effects in ceramic composite strength;Zok;J Mech Phys Solids,2021

3. Woven ceramic matrix composite surrogate model based on physics-informed recurrent neural network;Borkowski;Compos Struct,2023

4. Advanced sandwich structures for thermal protection systems in hypersonic vehicles: A review;Le;Compos B,2021

5. Research on high-temperature aerospace materials at NASA glenn research center;Dever Joyce;J Aerosp Eng,2013

Cited by 1 articles. 订阅此论文施引文献订阅此论文施引文献，注册后可以免费订阅5篇论文的施引文献，订阅后可以查看论文全部施引文献

1. Thermomechanical-induced cracking model for ceramic matrix composite laminates subjected to thermal gradients and transients;International Journal of Solids and Structures;2024-08

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