Experimental and Computational Evaluation of Small Microcoaxial Rotor in Hover-Reference-Cited by-同舟云学术

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Experimental and Computational Evaluation of Small Microcoaxial Rotor in Hover

Published:2011-01 Issue:1 Volume:48 Page:220-229
ISSN:0021-8669
Container-title:Journal of Aircraft
language:en
Short-container-title:Journal of Aircraft

Author:

Liu Z.¹,Albertani R.²,Moschetta J. M.³,Thipyopas C.⁴,Xu M.⁵

Affiliation:

1. University of Toulouse, 31400 Toulouse, France

2. University of Florida, Gainesville, Florida 32611

3. Institut Supérieur de l’ Aéronautique et de l’ Espace, 31055 Toulouse Cedex 4, France

4. Kasetsart University, 10900 Bangkok, Thailand

5. Northwestern Polytechnical University, 710072 Xi ’ an, People ’ s Republic of China

Publisher

American Institute of Aeronautics and Astronautics (AIAA)

Subject

Aerospace Engineering

Link

http://arc.aiaa.org/doi/pdf/10.2514/1.C031068

Reference41 articles.

1. Challenges Facing Future Micro-Air-Vehicle Development

2. Design, Analysis and Hover Performance of a Rotary Wing Micro Air Vehicle

3. From Natural Flyers to the Mechanical Realization of a Flapping Wing Micro Air Vehicle

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