12th International Energy Conversion Engineering Conference 2014
DOI: 10.2514/6.2014-3861
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Modeling Vertical-Axis Wind Turbine Performance: Blade Element Method vs. Finite Volume Approach

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Cited by 5 publications
(3 citation statements)
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“…While vertical axis turbines do offer significant operational advantages, their development has been hampered by the difficulty of modelling the associated aerodynamics as well as their rotational kinematics. Article [16] presents the results of a simulation of the baseline VAWT calculated using Star-CCM+, the finite volume method (FVM), and compares them with data obtained from a model with several flow tubes. Limitations of the pipe jet model suggest a low gear ratio because the model cannot reproduce the flow splitting and reattaching cycles that reduce space at high rotation angles.…”
Section: Orthogonal Turbines-review Of Sourcesmentioning
confidence: 99%
“…While vertical axis turbines do offer significant operational advantages, their development has been hampered by the difficulty of modelling the associated aerodynamics as well as their rotational kinematics. Article [16] presents the results of a simulation of the baseline VAWT calculated using Star-CCM+, the finite volume method (FVM), and compares them with data obtained from a model with several flow tubes. Limitations of the pipe jet model suggest a low gear ratio because the model cannot reproduce the flow splitting and reattaching cycles that reduce space at high rotation angles.…”
Section: Orthogonal Turbines-review Of Sourcesmentioning
confidence: 99%
“…Although the dynamic stall was early documented by Kramer, 1 it is still an interesting topic among aerodynamicists due to its massive effects on aerodynamic and structural performance. These effects were observed by a series of research leading to challenging applications, including helicopter rotor blades, 25 highly maneuverable fixed-wing aircrafts, 6 wind turbines, 79 compressor, 1014 flapping wings, 1521 and laminar separation flutter. 2224 Figure 1 shows an illustration of static and dynamic stall over an airfoil surface at an angle of attack ranging from small to high values.…”
Section: Introductionmentioning
confidence: 98%
“…It also stated that the turbulence models produce more accurate results at lower tip-speed ratios. Analysis of blade-vortex interaction (BVI) and its effect on the fluid flow as the blade passes through its own wake from the previous passage showed this effect was significant even for rotor-level loads (Kozak et al, 2014;Posa and Balaras, 2018).…”
Section: Introductionmentioning
confidence: 99%