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Vortex-induced vibration on a low mass ratio cylinder with a nonlinear dissipative oscillator at moderate Reynolds number
Institution:1. Institute of Launch Dynamics, Nanjing University of Science and Technology, Nanjing 210094, China;2. China Ship Development and Design Center, Wuhan 430064, China;3. School of Engineering, Aerospace Engineering and Aviation Discipline, RMIT University, Melbourne, VIC 3000, Australia;1. Institute of Launch Dynamics, Nanjing University of Science and Technology, Nanjing 210094, China;2. China Ship Development and Design Center, Wuhan 430064, China;3. School of Engineering, Aerospace Engineering and Aviation Discipline, RMIT University, Melbourne, VIC 3000 Australia;1. Department of Civil Engineering, School of Naval Architecture, Ocean and Civil Engineering, Shanghai Jiao Tong University, No. 800, Dongchuan Road, Shanghai 200240, China;2. State Key Laboratory of Ocean Engineering, Shanghai Jiao Tong University, No. 800, Dongchuan Road, Shanghai 200240, China;3. Collaborative Innovation Center for Advanced Ship and Deep-Sea Exploration, No. 800, Dongchuan Road, Shanghai 200240, China;4. College of Civil Engineering and Mechanics, Xiangtan University, Xiangtan 411105, China;5. Department of Aeronautics, Imperial College London, London SW7 2AZ, UK;6. Cullen College of Engineering, University of Houston, Houston, TX 77204, USA
Abstract:
Keywords:Non-linear energy sink  Vortex-induced vibrations  Overset mesh technology  Low mass ratio  Flow–cylinder–NES coupled system
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