Self-Excited Instability of Closed-Type Swirl Injector with Varying Conditions
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Jeong, Seokgyu | - |
dc.contributor.author | Bae, Jinhyun | - |
dc.contributor.author | Chung, Yunjae | - |
dc.contributor.author | Yoon, Sam S. | - |
dc.contributor.author | Yoon, Youngbin | - |
dc.date.accessioned | 2021-08-31T08:56:05Z | - |
dc.date.available | 2021-08-31T08:56:05Z | - |
dc.date.created | 2021-06-18 | - |
dc.date.issued | 2020-03 | - |
dc.identifier.issn | 0748-4658 | - |
dc.identifier.uri | https://scholar.korea.ac.kr/handle/2021.sw.korea/57528 | - |
dc.description.abstract | The dynamic characteristic of an injector is important for improving engine characteristics and preventing instability. In this study, the experiments on the unstable flow of a closed-type swirl injector were conducted, and the dynamic characteristic analysis of the relationship between internal and external flows was discussed. Consequently, it was found that the unstable characteristics of internal and external flows were similar. Main geometric parameters affecting the injector self-excited instability were also investigated. The fluctuating amplitude was mainly related to the momentum of the flow. On the other hand, the instability frequency was related to the axial velocity inside the swirl injector. Experiments with external pulsation were carried out to investigate the effect of the instability frequency in real environments. It was observed that the mean breakup length reduced by 25%, and the fluctuation amplitude of the spray angle increased more than twice compared with the out of tuned case. The results of this study can be an inspiration to engine design, considering the dynamic characteristics of an injector. | - |
dc.language | English | - |
dc.language.iso | en | - |
dc.publisher | AMER INST AERONAUTICS ASTRONAUTICS | - |
dc.subject | AERODYNAMIC INSTABILITY | - |
dc.subject | DYNAMIC CHARACTERISTICS | - |
dc.subject | PERIODIC ATOMIZATION | - |
dc.subject | COMBUSTION | - |
dc.title | Self-Excited Instability of Closed-Type Swirl Injector with Varying Conditions | - |
dc.type | Article | - |
dc.contributor.affiliatedAuthor | Yoon, Sam S. | - |
dc.identifier.doi | 10.2514/1.B37618 | - |
dc.identifier.scopusid | 2-s2.0-85081084083 | - |
dc.identifier.wosid | 000518624100013 | - |
dc.identifier.bibliographicCitation | JOURNAL OF PROPULSION AND POWER, v.36, no.2, pp.285 - 293 | - |
dc.relation.isPartOf | JOURNAL OF PROPULSION AND POWER | - |
dc.citation.title | JOURNAL OF PROPULSION AND POWER | - |
dc.citation.volume | 36 | - |
dc.citation.number | 2 | - |
dc.citation.startPage | 285 | - |
dc.citation.endPage | 293 | - |
dc.type.rims | ART | - |
dc.type.docType | Article | - |
dc.description.journalClass | 1 | - |
dc.description.journalRegisteredClass | scie | - |
dc.description.journalRegisteredClass | scopus | - |
dc.relation.journalResearchArea | Engineering | - |
dc.relation.journalWebOfScienceCategory | Engineering, Aerospace | - |
dc.subject.keywordPlus | AERODYNAMIC INSTABILITY | - |
dc.subject.keywordPlus | DYNAMIC CHARACTERISTICS | - |
dc.subject.keywordPlus | PERIODIC ATOMIZATION | - |
dc.subject.keywordPlus | COMBUSTION | - |
Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.
(02841) 서울특별시 성북구 안암로 14502-3290-1114
COPYRIGHT © 2021 Korea University. All Rights Reserved.
Certain data included herein are derived from the © Web of Science of Clarivate Analytics. All rights reserved.
You may not copy or re-distribute this material in whole or in part without the prior written consent of Clarivate Analytics.