2016
DOI: 10.2514/1.j054199
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Coriolis Effect on Dynamic Stall in a Vertical Axis Wind Turbine

Abstract: The immersed boundary method is used to simulate the flow around a two-dimensional cross section of a rotating NACA 0018 airfoil in order to investigate the dynamic stall occurring on a vertical axis wind turbine. The influence of dynamic stall on the force is characterized as a function of tip-speed ratio and Rossby number. The influence of the Coriolis effect is isolated by comparing the rotating airfoil to one undergoing an equivalent planar motion that is composed of surging and pitching motions that produ… Show more

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Cited by 45 publications
(14 citation statements)
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“…12 As presented in Dunne et al, 13 the computational results have a good agreement with experiments performed by Dunne and McKeon. 14 Current study aims at numerically investigating the self-starting capability of a VAWT using the immersed boundary projection method.…”
Section: Introductionsupporting
confidence: 81%
“…12 As presented in Dunne et al, 13 the computational results have a good agreement with experiments performed by Dunne and McKeon. 14 Current study aims at numerically investigating the self-starting capability of a VAWT using the immersed boundary projection method.…”
Section: Introductionsupporting
confidence: 81%
“…The empirically determined functional dependencies were used for the Reynolds number term and for the dynamic effects, where is given by (3.4) and can be found using the functional relationship given by (3.3) and shown in Figure 7. Variations in and drove unsteady effects such as dynamic stall, Coriolis and centrifugal forces as well as wake–blade interactions (see for example Rezaeiha, Montazeri, & Blocken, 2018; Tsai & Colonius, 2016). Given this, a variation in the Reynolds number appeared to only affect the quasisteady physics of the VAWT, such as airfoil boundary layer development, while leaving the dynamic phenomena unaltered.…”
Section: Resultsmentioning
confidence: 99%
“…The breadth of this parameter space suggests optimization by reduced-order models, but this is complicated by the unsteady nature of cross-flow turbine fluid dynamics. The blade's angle of attack varies throughout the turbine's rotation, potentially inducing dynamic stall 16,17 , and the blades pass disturbed flow during their downstream sweep, potentially interacting with coherent structures. Such dynamics are difficult to generalize to the full range of rotor geometries.…”
Section: Introductionmentioning
confidence: 99%
“…Unlike blade element momentum (BEM) models for axial-flow turbines 18 , analytical models [19][20][21] are often only valid for a specific configuration. Similarly, the challenges of simulating unsteady boundary layer dynamics 16,17 , combined with a lack of exploitable circumferential symmetry and a necessity for high spatial and temporal resolution 22 , make accurate two-dimensional simulations computationally expensive. Threedimensional simulations, which are even more expensive, are required to fully incorporate the effects of span-wise flow, mixing, and parasitic torque from blade supports [23][24][25] .…”
Section: Introductionmentioning
confidence: 99%