Art

J-GLOBAL ID：201802271200272188   Reference number：18A1061271

Experimental Study for Aerodynamic Performance of Quadrotor Helicopter

クワッドローターヘリコプタの空力性能に関する実験的研究

Author (3)： NGUYEN Duc Hung (Department of Aerospace Engineering, Nagoya University) ,  LIU Yu (Department of Aerospace Engineering, Nagoya University) ,  MORI Koichi (Department of Aerospace Engineering, Nagoya University)
Material： Transactions of the Japan Society for Aeronautical and Space Sciences (Web)  (Trans Jpn Soc Aeronaut Space Sci (Web))
Volume： 61  Issue： 1  Page： 29-39(J-STAGE)  Publication year： 2018 
JST Material Number： U0630A  ISSN： 2189-4205  Document type： Article
Article type： 原著論文  Country of issue： Japan (JPN)  Language： ENGLISH (EN)

Thesaurus term： rotor craft ,  *wind tunnel test ,  *aerodynamic characteristic ,  drag coefficient ,  Reynolds number ,  aerodynamic interference ,  series connection ,  thrust ,  uniform flow ,  forward flight ,  *quadrotor ,  low Reynolds number
Semi thesaurus term： wind tunnel experiment ,  tandem ,  前進率

Author keywords (5)： Quadrotor Helicopter ,  Momentum Theory ,  Blade Element Theory ,  Thrust Coefficient ,  Interference Effect

JST classification (1)： Aerodynamics of aircrafts  (QK02010T)

Reference (12)：

• 1) Johnson, W.: Rotorcraft Aeromechanics, Cambridge University Press, 2013, pp. 152–193.
• 2) Pounds, P.: Construction and Control of a Large Quadrotor Micro Air Vehicle, ANU PhD Thesis, September 2007.
• 3) Bangura, M. and Mahony, R.: Nonlinear Dynamic Modeling for High Performance Control of a Quadrotor, Proceedings of Australasian Conference on Robotics and Automation, Dec 2012.
• 4) O’Meara, M. and Mueller, T. J.: Laminar Separation Bubble Characteristics on an Airfoil at Low Reynolds Numbers, AIAA J., 8 (1987), pp. 1033–1041.
• 5) Kunz, P. J.: Aerodynamics and Design for Ultra-Low Reynolds Number Flight, Ph.D. Thesis, Stanford University, 2003.

Terms in the title (2)： 空力性能 ,  実験的研究