Blade geometric modification is one favorite way of enhancing the performance of vertical axis turbines. In this regard, V-shaped blades are a novel design featuring some leading-edge sweep angle. Currently, the relevant literature only focuses on finding the optimum parameters of the V-shaped blades and lacks a deep understanding of how they alter flow structure and whether they offer any performance improvement compared to other conventional types. To this aim, using three-dimensional numerical simulations, the flow structure and performance of two different V-shaped blade turbines, twisted and untwisted, are compared with straight and helicalblade turbines at tip speed ratios (TSRs) ranging from 0.69 to 1.5. Turbine torque average and fluctuation amplitude are chosen as the performance metrics. It is shown that the sweeping configuration of the V-shaped and helical types causes an inevitable spanwise flow, resulting in a performance loss, which makes neither type of V-shaped blade turbine advantageous at low TSRs.
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Univ Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, EnglandUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
He, Wei
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Zhang, Kai
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Rutgers State Univ, Dept Mech & Aerosp Engn, Piscataway, NJ 08854 USAUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Zhang, Kai
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Theofilis, Vassilios
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Univ Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Univ Sao Paulo, Escola Politecn, BR-5508900 Sao Paulo, SP, BrazilUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Theofilis, Vassilios
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Taira, Kunihiko
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Univ Calif Los Angeles, Dept Mech & Aerosp Engn, Los Angeles, CA 90095 USAUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Taira, Kunihiko
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Amitay, Michael
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Rensselaer Polytech Inst, Dept Mech Aeronaut & Nucl Engn, Troy, NY 12180 USAUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
机构:
Univ Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, EnglandUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
He, Wei
;
Zhang, Kai
论文数: 0引用数: 0
h-index: 0
机构:
Rutgers State Univ, Dept Mech & Aerosp Engn, Piscataway, NJ 08854 USAUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Zhang, Kai
;
Theofilis, Vassilios
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h-index: 0
机构:
Univ Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Univ Sao Paulo, Escola Politecn, BR-5508900 Sao Paulo, SP, BrazilUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Theofilis, Vassilios
;
Taira, Kunihiko
论文数: 0引用数: 0
h-index: 0
机构:
Univ Calif Los Angeles, Dept Mech & Aerosp Engn, Los Angeles, CA 90095 USAUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England
Taira, Kunihiko
;
Amitay, Michael
论文数: 0引用数: 0
h-index: 0
机构:
Rensselaer Polytech Inst, Dept Mech Aeronaut & Nucl Engn, Troy, NY 12180 USAUniv Liverpool, Dept Mech Mat & Aerosp Engn, Liverpool L69 3GH, Merseyside, England