2016
DOI: 10.1016/j.energy.2016.05.012
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Influences of yaw angle and turbulence intensity on the performance of a 20 kW in-stream hydrokinetic turbine

Abstract: Three-dimensional transient Computational Fluid Dynamics (CFD) simulations are performed to study the hydrodynamic performance of an ocean current turbine with a 3.0 m diameter 3-bladed rotor. Simulations are based on the Reynolds Averaged Navier-Stokes (RANS) equations and the shear stress transport k-ω turbulent model is utilized. The influence of yaw angle and upstream turbulence intensity (TI) on the turbine performance is studied. The CFD method is first validated using existing experimental data and good… Show more

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Cited by 52 publications
(28 citation statements)
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References 21 publications
(30 reference statements)
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“…This simulated 0.8 m rotor is designed to match the one used in experimental setup in Mycek et al (2014). Further validation of the CFD approach utilized here was carried by comparing the CFD approach with experimental setup in Bahaj et al (2007a, b) and is provided in detail in Tian et al (2016).…”
Section: Data Generation Methodologymentioning
confidence: 98%
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“…This simulated 0.8 m rotor is designed to match the one used in experimental setup in Mycek et al (2014). Further validation of the CFD approach utilized here was carried by comparing the CFD approach with experimental setup in Bahaj et al (2007a, b) and is provided in detail in Tian et al (2016).…”
Section: Data Generation Methodologymentioning
confidence: 98%
“…Using the data generation methodology described above, simulations are carried out for a reference 20 kW three bladed OCT model, with rotor diameter 3 m and hub diameter 0.6 m. The airfoil shapes used by this rotor are created from the FF-77-W airfoil type and other rotor details are available in Tian et al (2016). In addition to the 3 m rotor utilized to create the primary results presented in this paper, a 0.8 m rotor is simulated using the same CFD approach to validate the wake profile generated from the methodology presented here.…”
Section: Data Generation Methodologymentioning
confidence: 99%
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“…A previous study shows that the change in the rotor forces is less than 7.4% when the yaw angle is smaller than 15°. 26 Therefore, the effect of yaw on the rotor forces is neglected and the rotor forces at zero yaw state are used in this model. The force vector of the rotor is found by and C 2 , respectively, and ½x y , y y , z y T is the location of rotor in the UMP-fixed frame.…”
mentioning
confidence: 99%