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Experimental investigation of helical Savonius rotor with a twist of 180°
Affiliation:1. School of Energy and Power Engineering, Jiangsu University, Zhenjiang 212013, China;2. St. Anthony Falls Laboratory, University of Minnesota, Minneapolis 55414, USA;3. School of Material Science and Engineering, Jiangsu University, Zhenjiang 212013, China;1. Curtin University Malaysia, Miri, Sarawak 98009, Malaysia;2. Indian Institute of Technology Ropar, Rupnagar, Punjab 140001, India;3. Indian Institute of Technology Guwahati, North Guwahati 781039, India;1. Faculty of New Sciences and Technologies, University of Tehran, Tehran, Iran;2. Department of Energy Technology, Aalborg University, Pontoppidanstraede 111, 9220, Aalborg East, Denmark;1. Mechanical Power Eng. Dept., Faculty of Engineering, Shebin El-Kom, Menufiya University, Egypt;2. Mechanical Department, Faculty of Engineering, Sinai University, Egypt;3. Mechanical Power Eng. Dept., Faculty of Engineering, Mansoura University, Egypt
Abstract:Conventional Savonius rotors have low performance such as low coefficient of power and low coefficient of torque. In order to increase this performance, a helical Savonius rotor with a twist of 180° is proposed. In this paper, we are interested in studying the aerodynamic behavior of the helical Savonius rotors installed in an open jet wind tunnel. Particularly we are interested in studying the influence of variation of Reynolds number and the overlap ratio on the performance of a modified Savonius rotor with aspect ratio of 1.57 at a Reynolds numbers equal to Re = 79,794, Re = 99,578, Re = 116,064 and Re = 147,059. Results conclude that the variation of Reynolds number and overlap ratio has an effect on the global characteristics of the helical Savonius rotor. A comparison between the helical one and the conventional one shows that the maximum power coefficient of the Savonius wind rotor is higher. This work is developed at Laboratory of Electro-Mechanical System (LASEM) of the National School of Engineers of Sfax (ENIS).
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