Full metadata record
DC Field | Value | Language |
---|---|---|
dc.contributor.author | 조진수 | - |
dc.date.accessioned | 2019-05-10T06:16:40Z | - |
dc.date.available | 2019-05-10T06:16:40Z | - |
dc.date.issued | 2019-02 | - |
dc.identifier.citation | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES, Page. 1-11 | en_US |
dc.identifier.issn | 2093-274X | - |
dc.identifier.issn | 2093-2480 | - |
dc.identifier.uri | https://link.springer.com/article/10.1007/s42405-018-0121-4 | - |
dc.identifier.uri | https://repository.hanyang.ac.kr/handle/20.500.11754/103846 | - |
dc.description.abstract | Themarket demand on business jets is growing fast. The Blended-Wing-Body (BWB) configuration is adapted to design highefficient 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 ofAOAand Mach number produces stronger shock and drag coefficient is increased due to wave drag. | en_US |
dc.language.iso | en | en_US |
dc.publisher | SPRINGER | en_US |
dc.subject | Blended-wing-body | en_US |
dc.subject | Business jet | en_US |
dc.subject | Aerodynamic analysis | en_US |
dc.subject | Parametric study | en_US |
dc.title | Aerodynamic Analysis and Parametric Study of the Blended Wing Body Type Business Jet | en_US |
dc.type | Article | en_US |
dc.identifier.doi | 10.1007/s42405-018-0121-4 | - |
dc.relation.page | 1-11 | - |
dc.relation.journal | INTERNATIONAL JOURNAL OF AERONAUTICAL AND SPACE SCIENCES | - |
dc.contributor.googleauthor | Choi, Hyunmin | - |
dc.contributor.googleauthor | Cho, Jinsoo | - |
dc.relation.code | 2019040154 | - |
dc.sector.campus | S | - |
dc.sector.daehak | COLLEGE OF ENGINEERING[S] | - |
dc.sector.department | DIVISION OF MECHANICAL ENGINEERING | - |
dc.identifier.pid | jscho | - |
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