3-08-1

[3-08-1-01] Numerical Investigate on Influence of the Blade Angle Imbalance on Aerodynamic and Instability Characteristic of Coaxilcopter

Wei WEI^1,3,4, Jinghan TU^1,4, *Zhifang Ke^1,2, Molei ZHAO¹, Qingkai MENG¹, Haitao ZHANG^1,4 (1. School of Mechanical Engineering, Beijing Institute of Technology, 100081, Beijing, China, 2. Institute of Advanced Technology, Beijing Institute of Technology, 250300, Jinan, Shandong, China, 3. National Key Laboratory of Vehicular Transmission, Beijing Institute of Technology, 100081, Beijing, China, 4. Chongqing Innovation Center, Beijing Institute of Technology, 401122, Chongqing, China)

キーワード：blade angle imbalance, angle of attack, coaxilcopter, aerodynamic, instability