Coupled Analysis of Thermo-Fluid-Flexible Multi-body Dynamics of a Two-Dimensional Engine Nozzle

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dc.contributor.authorEun, WonJongko
dc.contributor.authorKim, JaeWonko
dc.contributor.authorKwon, Oh-Joonko
dc.contributor.authorChung, Chanhoonko
dc.contributor.authorShin, Sang-Joonko
dc.contributor.authorBauchau, Olivier A.ko
dc.date.accessioned2017-06-05T02:21:07Z-
dc.date.available2017-06-05T02:21:07Z-
dc.date.created2017-05-29-
dc.date.created2017-05-29-
dc.date.issued2017-03-
dc.identifier.citationINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, v.18, no.1, pp.70 - 81-
dc.identifier.issn2093-274X-
dc.identifier.urihttp://hdl.handle.net/10203/223925-
dc.description.abstractVarious components of an engine nozzle are modeled as flexible multi-body components that are operated under high temperature and pressure. In this paper, in order to predict complex behavior of an engine nozzle, thermo-fluid-flexible multi body dynamics coupled analysis framework was developed. Temperature and pressure on the nozzle wall were obtained by the steady-state flow analysis for a two-dimensional nozzle. The pressure and temperature-dependent material properties were delivered to the flexible multi-body dynamics analysis. Then the deflection and strain distribution for a nozzle configuration was obtained. Heat conduction and thermal analyses were done using MSC.NASTRAN. The present framework was validated for a simple nozzle configuration by using a one-way coupled analysis. A two-way coupled analysis was also performed for the simple nozzle with an arbitrary joint clearance, and an asymmetric flow was observed. Finally, the total strain result for a realistic nozzle configuration was obtained using the one-way and two-way coupled analyses.-
dc.languageEnglish-
dc.publisherKOREAN SOC AERONAUTICAL & SPACE SCIENCES-
dc.titleCoupled Analysis of Thermo-Fluid-Flexible Multi-body Dynamics of a Two-Dimensional Engine Nozzle-
dc.typeArticle-
dc.identifier.wosid000400307000009-
dc.identifier.scopusid2-s2.0-85021056424-
dc.type.rimsART-
dc.citation.volume18-
dc.citation.issue1-
dc.citation.beginningpage70-
dc.citation.endingpage81-
dc.citation.publicationnameINTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES-
dc.identifier.doi10.5139/1JASS.2017.18.1.70-
dc.contributor.localauthorKwon, Oh-Joon-
dc.contributor.nonIdAuthorEun, WonJong-
dc.contributor.nonIdAuthorChung, Chanhoon-
dc.contributor.nonIdAuthorShin, Sang-Joon-
dc.contributor.nonIdAuthorBauchau, Olivier A.-
dc.description.isOpenAccessN-
dc.type.journalArticleArticle-
dc.subject.keywordAuthorMulti-body dynamics-
dc.subject.keywordAuthorFluid-flexible multi-body dynamics coupled analysis-
dc.subject.keywordAuthorCoupled analysis framework-
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AE-Journal Papers(저널논문)
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