Aerodynamic Analysis and Parametric Study of the Blended-Wing-Body-Type Business Jet
DC Field | Value | Language |
---|---|---|
dc.contributor.author | Choi, Hyunmin | - |
dc.contributor.author | Cho, Jinsoo | - |
dc.date.accessioned | 2021-08-02T11:30:05Z | - |
dc.date.available | 2021-08-02T11:30:05Z | - |
dc.date.created | 2021-05-12 | - |
dc.date.issued | 2019-06 | - |
dc.identifier.issn | 2093-274X | - |
dc.identifier.uri | https://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/13451 | - |
dc.description.abstract | The market demand on business jets is growing fast. The Blended-Wing-Body (BWB) configuration is adapted to design high-efficient green business jet. Conceptual study of the BWB-type transonic business jet is carried out. The BWB-type business jet expected to provide a better cabin space and aerodynamic performance to compare with the conventional business jet. An aerodynamic analysis of the BWB-type transonic business jet is performed to understand the flow field around the aircraft at a high subsonic flight speed. The commercial CFD (Computational Fluid Dynamics) code, ANSYS Fluent, is used for aerodynamic analysis. A parametric study is carried out to analyze the relation between the design parameters and aerodynamic characteristics. The commercial PIDO (Process Integration and Design Optimization) tool, PIAnO, is used to perform a parametric study. As a result of parametric study, the sensitivity of the design parameters is analyzed and a proportion of aerodynamic influence of each design parameter is presented. One of the sample design configurations for detailed aerodynamic analysis is selected. As a result of the aerodynamic analysis, aerodynamic coefficients and pressure coefficient distribution around the BWB-type business jet are presented. Increase of AOA and Mach number produces stronger shock and drag coefficient is increased due to wave drag. | - |
dc.language | 영어 | - |
dc.language.iso | en | - |
dc.publisher | SPRINGER | - |
dc.title | Aerodynamic Analysis and Parametric Study of the Blended-Wing-Body-Type Business Jet | - |
dc.type | Article | - |
dc.contributor.affiliatedAuthor | Cho, Jinsoo | - |
dc.identifier.doi | 10.1007/s42405-018-0121-4 | - |
dc.identifier.scopusid | 2-s2.0-85066320655 | - |
dc.identifier.wosid | 000469385300002 | - |
dc.identifier.bibliographicCitation | International Journal of Aeronautical and Space Sciences, v.20, no.2, pp.335 - 345 | - |
dc.relation.isPartOf | International Journal of Aeronautical and Space Sciences | - |
dc.citation.title | International Journal of Aeronautical and Space Sciences | - |
dc.citation.volume | 20 | - |
dc.citation.number | 2 | - |
dc.citation.startPage | 335 | - |
dc.citation.endPage | 345 | - |
dc.type.rims | ART | - |
dc.type.docType | Article | - |
dc.identifier.kciid | ART002475871 | - |
dc.description.journalClass | 1 | - |
dc.description.isOpenAccess | N | - |
dc.description.journalRegisteredClass | scie | - |
dc.description.journalRegisteredClass | scopus | - |
dc.description.journalRegisteredClass | kci | - |
dc.relation.journalResearchArea | Engineering | - |
dc.relation.journalWebOfScienceCategory | Engineering, Aerospace | - |
dc.subject.keywordPlus | DESIGN | - |
dc.subject.keywordAuthor | Blended-wing-body | - |
dc.subject.keywordAuthor | Business jet | - |
dc.subject.keywordAuthor | Aerodynamic analysis | - |
dc.subject.keywordAuthor | Parametric study | - |
dc.identifier.url | https://link.springer.com/article/10.1007/s42405-018-0121-4 | - |
Items in ScholarWorks are protected by copyright, with all rights reserved, unless otherwise indicated.
222, Wangsimni-ro, Seongdong-gu, Seoul, 04763, Korea+82-2-2220-1365
COPYRIGHT © 2021 HANYANG UNIVERSITY.
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.