A study on thermal behaviour of thermal barrier coating: investigation of particle size, YSZ/polysilazane, time and temperature curing effect-Reference-Cited by-同舟云学术

A study on thermal behaviour of thermal barrier coating: investigation of particle size, YSZ/polysilazane, time and temperature curing effect

Published:2024 Issue:34 Volume:14 Page:24687-24702
ISSN:2046-2069
Container-title:RSC Advances
language:en
Short-container-title:RSC Adv.

Author:

Widyastuti ¹^ORCID,Zulfa Liyana Labiba²,Rizaldi Wafiq Azhar¹^ORCID,Azhar Jauhari¹,Safrida Ninik¹,Pratama Azzah Dyah¹,Wahyuono Ruri Agung³,Sulistijono ¹,Fajarin Rindang¹,Hakim Arif Nur⁴

Affiliation:

1. Department of Materials and Metallurgical Engineering, Faculty of Industrial Technology and Systems Engineering, Institut Teknologi Sepuluh Nopember, Jl. Arif Rahman Hakim, Kampus ITS Keputih-Sukolilo, Surabaya 60111, Indonesia

2. Department of Chemistry, Faculty of Science and Data Analytics, Institut Teknologi Sepuluh Nopember, Jl. Arif Rahman Hakim, Kampus ITS Keputih-Sukolilo, Surabaya 60111, Indonesia

3. Department of Engineering Physics, Faculty of Industrial Technology and Systems Engineering, Institut Teknologi Sepuluh Nopember, Jl. Arif Rahman Hakim, Kampus ITS Keputih-Sukolilo, Surabaya 60111, Indonesia

4. National Research and Innovation Agency, Tangerang 15314, Indonesia

Abstract

Thermal conductivity and adhesion strength effects were studied for thermal barrier coatings (TBCs) with different particle sizes, YSZ content, time, and temperature curing.

Funder

Badan Riset dan Inovasi Nasional

Publisher

Royal Society of Chemistry (RSC)

Link

http://pubs.rsc.org/en/content/articlepdf/2024/RA/D4RA03620D

Reference78 articles.

1. Light-weighting in aerospace component and system design

2. Investigation on the effectiveness of silane-based field level surface treatments of aluminum substrates for on-aircraft bonded repairs

3. Part distortion optimization of aluminum-based aircraft structures using finite element modeling and artificial neural networks

4. Crack path of in-service fatigued fan titanium disk of D-18T gas-turbine engine of the aircraft An-124