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dc.contributor.authorPraveen, Kandasamy-
dc.contributor.authorKim, Heejin-
dc.contributor.authorLee, Juhyeong-
dc.contributor.authorCha, Ji-Hyun-
dc.contributor.authorLee, Min Wook-
dc.date.accessioned2025-12-23T06:30:05Z-
dc.date.available2025-12-23T06:30:05Z-
dc.date.created2025-12-19-
dc.date.issued2026-02-
dc.identifier.issn1359-835X-
dc.identifier.urihttps://pubs.kist.re.kr/handle/201004/153851-
dc.description.abstractDeveloping ceramic-based thermal barrier coatings (TBCs) on the fabric materials is challenging because they lack stable surfaces for achieving high-quality coatings. Herein, we propose the direct deposition of TBCs on the surface of carbon fabric, followed by the manufacturing of carbon fiber-reinforced plastic (CFRP) composite and the evaluation of its high-temperature performance. Yttrium aluminum garnet (YAG) TBCs were deposited on 3 K carbon fabric (CF) using atmospheric plasma spray (APS). The porosity of the coatings was tailored using a poreforming agent, polyether ether ketone (PEEK), and the CFRP composite was manufactured through the vacuumassisted resin transfer molding (VARTM) process. The thermal barrier performance of the resulting CFRP-TBC composite was evaluated at various temperatures, and its mechanical properties were also assessed. The porous YAG TBC, with a porosity of approximately 35 %, exhibited a reduced thermal conductivity of 0.57-0.64 W/m & sdot;K in the 25-400 degrees C range. The thermal barrier performance tests revealed that the back-surface temperature of the CFRP-TBC composite specimen ranged from 253 to 305 degrees C, while the flame temperature was approximately 500-700 degrees C. The composite maintained its initial strength up to 500 degrees C and retained about 25 % even after exposure to 700 degrees C. This study demonstrates the feasibility of integrating porous YAG TBCs directly onto CFs to enhance the high-temperature resistance of CFRP composites while maintaining manufacturability through conventional VARTM processing.-
dc.languageEnglish-
dc.publisherPergamon Press Ltd.-
dc.titleHigh-performance ceramic thermal barrier coatings for carbon fiber-reinforced plastics developed by atmospheric plasma spraying-
dc.typeArticle-
dc.identifier.doi10.1016/j.compositesa.2025.109424-
dc.description.journalClass3-
dc.identifier.bibliographicCitationComposites Part A: Applied Science and Manufacturing, v.201-
dc.citation.titleComposites Part A: Applied Science and Manufacturing-
dc.citation.volume201-
dc.description.isOpenAccessY-
dc.identifier.wosid001621888100002-
dc.identifier.scopusid2-s2.0-105021939050-
dc.relation.journalWebOfScienceCategoryEngineering, Manufacturing-
dc.relation.journalWebOfScienceCategoryMaterials Science, Composites-
dc.relation.journalResearchAreaEngineering-
dc.relation.journalResearchAreaMaterials Science-
dc.type.docTypeArticle-
dc.subject.keywordPlusYTTRIUM-ALUMINUM-GARNET-
dc.subject.keywordPlusADHESION STRENGTH-
dc.subject.keywordPlusPVD COATINGS-
dc.subject.keywordPlusBOND COAT-
dc.subject.keywordPlusCONDUCTIVITY-
dc.subject.keywordPlusBEHAVIOR-
dc.subject.keywordPlusEROSION-
dc.subject.keywordPlusTEMPERATURE-
dc.subject.keywordPlusOXIDATION-
dc.subject.keywordPlusPOLYMERS-
dc.subject.keywordAuthorPlasma spray-
dc.subject.keywordAuthorCarbon fabric-
dc.subject.keywordAuthorThermal conductivity-
dc.subject.keywordAuthorMechanical properties-
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