Cited 10 time in
Effect of Annealing and Crack Orientation on Fatigue Crack Propagation of Ti64 Alloy Fabricated by Direct Energy Deposition Process
| DC Field | Value | Language |
|---|---|---|
| dc.contributor.author | Kim, Soyoung | - |
| dc.contributor.author | Oh, Hojun | - |
| dc.contributor.author | Kim, Jung Gi | - |
| dc.contributor.author | Kim, Sangshik | - |
| dc.date.accessioned | 2022-12-26T07:40:50Z | - |
| dc.date.available | 2022-12-26T07:40:50Z | - |
| dc.date.issued | 2022-01 | - |
| dc.identifier.issn | 1598-9623 | - |
| dc.identifier.issn | 2005-4149 | - |
| dc.identifier.uri | https://scholarworks.gnu.ac.kr/handle/sw.gnu/1784 | - |
| dc.description.abstract | Effects of annealing condition and crack orientation on fatigue crack propagation (FCP) behavior of DED (direct energy deposition)-processed Ti-6Al-4V (Ti64) specimens were studied. It was found that the FCP resistance of Ti64 increased significantly with annealing, particularly above beta transus temperature, due to the microstructural coarsening inducing less damage accumulation at the tip of crack. The FCP behavior of as-built and as-annealed DED Ti64 specimens was isotropic with crack direction either parallel or perpendicular to building direction. The detailed micrographic and fractographic analyses on FCP-tested specimens suggested that the presence of largely elongated beta grain boundaries did not affect the advance of crack. | - |
| dc.format.extent | 11 | - |
| dc.language | 영어 | - |
| dc.language.iso | ENG | - |
| dc.publisher | 대한금속·재료학회 | - |
| dc.title | Effect of Annealing and Crack Orientation on Fatigue Crack Propagation of Ti64 Alloy Fabricated by Direct Energy Deposition Process | - |
| dc.type | Article | - |
| dc.publisher.location | 대한민국 | - |
| dc.identifier.doi | 10.1007/s12540-021-01087-3 | - |
| dc.identifier.scopusid | 2-s2.0-85116362521 | - |
| dc.identifier.wosid | 000703394300001 | - |
| dc.identifier.bibliographicCitation | Metals and Materials International, v.28, no.1, pp 205 - 215 | - |
| dc.citation.title | Metals and Materials International | - |
| dc.citation.volume | 28 | - |
| dc.citation.number | 1 | - |
| dc.citation.startPage | 205 | - |
| dc.citation.endPage | 215 | - |
| dc.type.docType | Article | - |
| dc.identifier.kciid | ART002799325 | - |
| dc.description.isOpenAccess | N | - |
| dc.description.journalRegisteredClass | scie | - |
| dc.description.journalRegisteredClass | scopus | - |
| dc.description.journalRegisteredClass | kci | - |
| dc.relation.journalResearchArea | Materials Science | - |
| dc.relation.journalResearchArea | Metallurgy & Metallurgical Engineering | - |
| dc.relation.journalWebOfScienceCategory | Materials Science, Multidisciplinary | - |
| dc.relation.journalWebOfScienceCategory | Metallurgy & Metallurgical Engineering | - |
| dc.subject.keywordPlus | MECHANICAL-PROPERTIES | - |
| dc.subject.keywordPlus | COOLING RATE | - |
| dc.subject.keywordPlus | GROWTH-BEHAVIOR | - |
| dc.subject.keywordPlus | TI-6AL-4V ALLOY | - |
| dc.subject.keywordPlus | MICROSTRUCTURE | - |
| dc.subject.keywordPlus | TITANIUM | - |
| dc.subject.keywordPlus | RESISTANCE | - |
| dc.subject.keywordPlus | POWDER | - |
| dc.subject.keywordPlus | AEROSPACE | - |
| dc.subject.keywordPlus | STRESS | - |
| dc.subject.keywordAuthor | Ti-6Al-4V | - |
| dc.subject.keywordAuthor | Direct energy deposition | - |
| dc.subject.keywordAuthor | Fatigue crack propagation | - |
| dc.subject.keywordAuthor | Annealing | - |
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