2016
DOI: 10.2514/1.b35550
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Modeling Vertical-Axis Wind-Turbine Performance: Blade-Element Method Versus Finite Volume Approach

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Cited by 12 publications
(8 citation statements)
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“…Wake interaction is the effect of the turbulent wakes generated by the front half blades on the rear half blades. By studying graphic visualizations of the vorticity generated by the blades, Kozal et al 21 proposed a formula to calculate the number of wakes, N ω = 0.85N b T SR. Each blade almost intersect with wake twice. By neglecting the wake diffusion, the wake length can be calculated, L wake = 2cN ω .…”
Section: Wake Interactionmentioning
confidence: 99%
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“…Wake interaction is the effect of the turbulent wakes generated by the front half blades on the rear half blades. By studying graphic visualizations of the vorticity generated by the blades, Kozal et al 21 proposed a formula to calculate the number of wakes, N ω = 0.85N b T SR. Each blade almost intersect with wake twice. By neglecting the wake diffusion, the wake length can be calculated, L wake = 2cN ω .…”
Section: Wake Interactionmentioning
confidence: 99%
“…In the Figure 6, the average power coefficient calculated by DMST with and without dynamic stall and wake correction is plotted with CFD result conducted by Kozak 21 . Kozak investigated the performance of the VAWT by using finite volume method simulation.…”
Section: Design Optimization Validationmentioning
confidence: 99%
See 1 more Smart Citation
“…This leads to the highly unsteady and nonlinear flow phenomenon known as dynamic stall (Simão Ferreira et al, 2009;Buchner et al, 2015Buchner et al, , 2018, which causes significant hysteresis in drag and lift forces. Lastly, depending on the tip speed ratio and rotor solidity, a blade located on the downwind rotor section may interact with its own or another blade's wake generated upwind (Kozak et al, 2016;Posa and Balaras, 2018), complicating further the VAWT response.…”
Section: Introductionmentioning
confidence: 99%
“…This leads to the highly unsteady and non-linear flow phenomenon known as dynamic stall (Simão Ferreira et al, 2009;Buchner et al, 2015Buchner et al, , 2018, which causes significant hysteresis in drag and lift forces. Lastly, depending on the tip speed ratio and rotor solidity, a blade located on the downwind rotor section may interact with its own or another blade's wake generated upwind (Kozak et al, 2016;Posa and Balaras, 2018), complicating further the VAWT response.…”
Section: Introductionmentioning
confidence: 99%