NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER ADVERSE SITUATIONS
學年 110
學期 1
發表日期 2021-09-06
作品名稱 NUMERICAL STUDY OF QUAD-ROTOR AIRCRAFT PERFORMANCE UNDER ADVERSE SITUATIONS
作品名稱（其他語言）
著者 Tung Wan; Meng-Han Tsai
作品所屬單位
出版者
會議名稱 32nd congress of the International Council of the Aeronautical Sciences
會議地點 上海市，中國
摘要 Unmanned Aerial Vehicles or UAVs are becoming more popular nowadays, and in-depth study of quad-copter UAV falls into detrimental situations required more investigations. In this work not only the aerodynamic parameters of quad-copter, but also the physical phenomenon for quad-copter flying under severe weather conditions are numerically simulated. An APC 10x4.7 rotor is first chosen as the validation benchmark case. Due to recent aviation safety concerns, the free-fall situation of quad-copter will be our major concern, and the worst realistic situations under severe weather condition are simulated, such as flying in the heavy rain and different typical gust wind conditions, for both the quad-copter hover and forward flight situations. It is found that the heavy rain effect is not as severe as the downdraft or the horizontal gust wind situations. It is hoped that this research can help the quad-copter UAV industries and academia to understand more about how adverse situations’ impact on quad-copter performance.
關鍵字 Quad-copter Performance;Terminal Velocity;Adverse Situations
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 20210906~20210910
通訊作者 Tung Wan
國別 CHN
公開徵稿
出版型式
出處 The proceedings of the 32nd International Council of the Aeronautical Sciences congress
相關連結

機構典藏連結 ( http://tkuir.lib.tku.edu.tw:8080/dspace/handle/987654321/121604 )