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Impact of flexibility on the aerodynamics of an aspect ratio two membrane wing
Institution:1. AFRL/RQVA, Bldg 146 Rm 225, 2210 Eighth St, Wright-Patterson AFB, OH 45433-7512, USA;2. School of Mechanical and Aerospace Engineering, University of Oklahoma, Norman, OK 73019-1052, USA;1. Hong Kong University of Science and Technology, Hong Kong;2. University of Southern California, United States of America;1. Computational Sciences Laboratory, UCY-CompSci, Department of Mechanical & Manufacturing Engineering, University of Cyprus, 75 Kallipoleos, Nicosia 1678, Cyprus;2. ONERA, The French Aerospace Lab, F-31055 Toulouse, France;1. Nephrology, Department of Clinical and Experimental Medicine, University of Catania, Catania, Italy;2. Internal Medicine, Department of Clinical and Experimental Medicine, University of Catania, Catania, Italy;1. Division of Orthopaedic Surgery, Schulich School of Medicine and Dentistry, The University of Western Ontario, London, Ontario, Canada;2. Faculty of Health Sciences, The University of Western Ontario, London, Ontario, Canada
Abstract:
Keywords:Membrane wing  Aeroelasticity  Micro air vehicle  Unsteady aerodynamics  Vortex dynamics
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