Design aspects of a CMC coating-like system for hot surfaces of aero engine components-Reference-Cited by-同舟云学术

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Design aspects of a CMC coating-like system for hot surfaces of aero engine components

Published:2024-02 Issue: Volume:14 Page:100251
ISSN:2666-3597
Container-title:Forces in Mechanics
language:en
Short-container-title:Forces in Mechanics

Author:

Canale Giacomo,Rubino Felice^ORCID,Citarella Roberto

Publisher

Elsevier BV

Reference49 articles.

1. Solid particle erosion behavior of melt-infiltrated SiC/SiC ceramic matrix composites (CMCs) in a simulated turbine engine environment;Panakarajupally;Compos. Part B Eng.,2021

2. CMC integration and demonstration for gas turbine engines (CINDERS);Barnard;Appl. Therm. Eng.,2004

3. Life assessment of thermomechanical fatigue in a woven SiC/SiC ceramic matrix composite with an environmental barrier coating at elevated temperature;Yang;Int. J. Fatigue,2023

4. Welding on Ni based super alloys–a review;Winowlin Jappes;Mater. Today Proc.,2022

5. Thermomechanical fatigue failure investigation on a single crystal nickel superalloy turbine blade;Wang;Eng. Fail. Anal.,2016

Cited by 2 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. Oxidation Driven Damage on SiC/BN/SiC Ceramic Matrix Composite Aero-Engine Structures: An Iterative Computational Framework;Materials;2024-06-20

2. Erosion behaviour of low-pressure cold-sprayed Ni coatings for concentrating solar power receivers;Surface Engineering;2024-04

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