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Loads and propulsive efficiency of a flexible airfoil performing sinusoidal deformations
Affiliation:1. IITB-Monash Research Academy, India;2. Department of Mechanical Engineering, Indian Institute of Technology Bombay, Powai, Mumbai 400076, India;3. Department of Mechanical Engineering, Monash University, 3800, Clayton, Australia;1. Department of Aerodynamics, Nanjing University of Aeronautics and Astronautics, Yudao Street 29, Nanjing, Jiangsu 210016, China;2. National Key Laboratory of Science and Technology on Hydrodynamics, China Ship Scientific Research Center, Wuxi, Jiangsu 214082, China;1. Laboratoire de Mathématiques (UMR 6620), Campus des Cézeaux, Université Blaise Pascal, B.P. 80026, 63171 Aubière cedex, France;2. Institut de Mathématiques de Toulouse, Unité Mixte C.N.R.S. 5219, Université Paul Sabatier Toulouse III, 118 route de Narbonne, 31062 Toulouse Cedex 9, France;1. Department of Mathematics and Statistics, Memorial University of Newfoundland, St. John׳s, NL, Canada A1C 5S7;2. Department of Mathematics, Middle East Technical University, Ankara, Turkey
Abstract:
Keywords:Flexible airfoil  Sinusoidal motion  State-space airloads theory  High Reynolds number
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