ON THE AERODYNAMIC ANASYSIS OF A MODERN ALL-ELECTRIC POWERED CE-LINER AIRCRAFT
學年 111
學期 1
發表日期 2022-09-04
作品名稱 ON THE AERODYNAMIC ANASYSIS OF A MODERN ALL-ELECTRIC POWERED CE-LINER AIRCRAFT
作品名稱（其他語言）
著者 Tung Wan; Po-Yu Huang
作品所屬單位
出版者
會議名稱 33rd International Council of the Aeronautical Sciences
會議地點 Stockholm, Sweden
摘要 The Ce-Liner aircraft developed by Bauhaus Luftfahrt is selected as our research target, and the C-wing assembly is based on a non-planar three-surface configuration: main wing, side wing and top wing. This work implement software to simulate whether Ce-Liner can reduce the generation and strength of wingtip vortices during cruise, and whether it can improve the efficiency of the aircraft with better economic benefits. Our findings revealed this Ce-Liner configuration can increase the lift-to-drag efficiency by about 20 percent during cruise. Also since it’s an all-electric aircraft, it can greatly reduce the weights of the turbofan engine and fuel, thus the high-lift devices can be eliminated. Furthermore, this Ce-Liner will not need to stock fuel in the main wing, hence the thickness and weight of the wing could be further reduced. In addition, it is found that this aircraft configuration has a stronger crosswind resistance capability due to our gust crosswind simulation.
關鍵字 Ce-Liner;All-Electric Aircraft;C-wing;Cross Wind
語言 en_US
收錄於
會議性質 國際
校內研討會地點 無
研討會時間 20220904~20220909
通訊作者 宛同
國別 SWE
公開徵稿
出版型式
出處 Proceeding of 33rd International Council of the Aeronautical Sciences
相關連結

機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/123828 )