Journal of Applied Mathematics and Physics

Vol.2 No.12(2014), Paper ID 51738, 8 pages

DOI:10.4236/jamp.2014.212117

 

Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion

 

Chunjin Yu, Daewon Kim, Yi Zhao

 

Institute of Flight Vehicle Engineering, Nanchang Hangkong University, Nanchang, China
Department of Aerospace Engineering, Embry-Riddle Aeronautical University, Daytona Beach, USA
Department of Aerospace Engineering, Embry-Riddle Aeronautical University, Daytona Beach, USA
Department of Aerospace Engineering, Embry-Riddle Aeronautical University, Daytona Beach, USA

 

Copyright © 2014 Chunjin Yu, Daewon Kim, Yi Zhao et al. This is an open access article distributed under the Creative Commons Attribution License, which permits unrestricted use, distribution, and reproduction in any medium, provided the original work is properly cited.

 

How to Cite this Article


Yu, C. , Kim, D. and Zhao, Y. (2014) Lift and Thrust Characteristics of Flapping Wing Aerial Vehicle with Pitching and Flapping Motion. Journal of Applied Mathematics and Physics, 2, 1031-1038. doi: 10.4236/jamp.2014.212117.

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