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Design and aerodynamic analysis of a flapping-wing micro aerial vehicle
Authors:Bor-Jang Tsai  Yu-Chun Fu
Institution:1. Department of Aerospace Engineering, Korea Advanced Institute of Science and Technology (KAIST), 291 Daehak-ro, Yuseong-gu, Daejeon 34141, Republic of Korea;2. Faculty of Aerospace Engineering, Le Quy Don Technical University, 236 Hoang Quoc Viet, Vietnam;1. Air Force Institute of Technology, Department of Aeronautics and Astronautics, 2950 Hobson Way, Wright-Patterson AFB, OH 45433, United States;2. Virginia Military Institute, Mechanical Engineering Department, 709 Nichols Hall, Lexington, VA 24450, United States;1. Engineering Mechanics Program, Viriginia Tech, 24061, USA;2. Department of Mechanical and Aerospace Engineering, University of Central Florida, Orlando, FL 32816-2450, USA;3. Mechanical and Aerospace Engineering, University of California, Irvine, CA 92697, USA;4. Department of Civil, Environmental and Ocean Engineering, Stevens Institute of Technology, 1 Castle Point Terrace, Hoboken, NJ 07030, USA;1. Centre for Aeronautics, Aerospace, Cranfield University, Cranfield, Beds, UK;2. School of Transport Science and Engineering, Beihang University, Beijing, China;3. School of Aerospace Engineering, Beijing Institute of Technology, Beijing, China;1. Department of Smart Vehicle Engineering and Artificial Muscle Research Center, Konkuk University, Seoul 05029, Republic of Korea;2. Department of Aerospace Information Engineering, Konkuk University, Seoul 05029, Republic of Korea
Abstract:
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