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Conceptual Design of the Blended Wing Body Type Business Jet

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dc.contributor.authorChoi, Hyunmin-
dc.contributor.authorRyu, Minhyung-
dc.contributor.authorKim, Jinuk-
dc.contributor.authorCho, Jin Soo-
dc.date.accessioned2024-12-20T06:20:27Z-
dc.date.available2024-12-20T06:20:27Z-
dc.date.issued2014-10-
dc.identifier.urihttps://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/202593-
dc.description.abstractThe demand on the business jet is growing fast. Conceptual study of the high efficient transonic business jet is carried out by using Blend-Wing-Body (BWB) configuration. The aerodynamic analysis of the BWB type transonic business jet is performed to understand the flow field around the aircraft at high subsonic flight speed. Commercial CFD code, ANSYS Fluent, is used for aerodynamic analysis of the BWB type business jet. As the results of aerodynamic study, the Mach number and pressure coefficient distribution around the BWB type business jet is presented.-
dc.format.extent2-
dc.language영어-
dc.language.isoENG-
dc.publisherInstitute of Fluid Science, Tohoku University-
dc.titleConceptual Design of the Blended Wing Body Type Business Jet-
dc.typeArticle-
dc.publisher.location일본-
dc.identifier.bibliographicCitationEleventh International Conference on Flow Dynamics, pp 116 - 117-
dc.citation.titleEleventh International Conference on Flow Dynamics-
dc.citation.startPage116-
dc.citation.endPage117-
dc.type.docTypeProceeding-
dc.description.isOpenAccessN-
dc.description.journalRegisteredClassother-
dc.identifier.urlhttp://www.ifs.tohoku.ac.jp/icfd2014/program/ICFD2014.pdf-
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