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Aerodynamic Analysis of Blended Wing Body Business Jet

Authors
Choi, HyunminLee, SeawookCho, Jin Soo
Issue Date
Nov-2013
Publisher
Institute of Fluid Science, Tohoku University
Citation
Tenth International Conference on Flow Dynamics, pp 140 - 141
Pages
2
Indexed
OTHER
Journal Title
Tenth International Conference on Flow Dynamics
Start Page
140
End Page
141
URI
https://scholarworks.bwise.kr/hanyang/handle/2021.sw.hanyang/202591
Abstract
Aerodynamic analysis of the BWB business jet is performed to analyze the flow field around the aircraft at high subsonic flight speed. Because of the cabin height, center body section is designed relatively thicker than general transonic airfoils. REA 5212 airfoil is selected for wing section. ANSYS Fluent is used for aerodynamic analysis of the BWB business jet. Because of the center body section produces less lift than wing section, strength of local shock on the center body is weaker than wing section. The weaker shock on the center body has advantage of locating the engine intake.
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서울 공과대학 > 서울 기계공학부 > 1. Journal Articles

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