2012
DOI: 10.1016/j.apenergy.2011.04.037
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Numerical modeling of an S809 airfoil under dynamic stall, erosion and high reduced frequencies

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Cited by 115 publications
(74 citation statements)
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“…Using the 'dynamic mesh' technique in CFD, unsteady aerodynamic loads associated with pitching motion [26,[28][29][30] as well as translational motion [27,31] of the airfoil can be simulated. This suggests the feasibility of using CFD techniques to investigate the effects of the vibration-induced unsteady velocity components of the airfoil on the aerodynamic loads.…”
Section: Dynamic Stallmentioning
confidence: 99%
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“…Using the 'dynamic mesh' technique in CFD, unsteady aerodynamic loads associated with pitching motion [26,[28][29][30] as well as translational motion [27,31] of the airfoil can be simulated. This suggests the feasibility of using CFD techniques to investigate the effects of the vibration-induced unsteady velocity components of the airfoil on the aerodynamic loads.…”
Section: Dynamic Stallmentioning
confidence: 99%
“…They found that the SST k-ω model was superior. Gharali and Johnson [30] simulated the dynamic stall of an S809 airfoil for several Reynolds numbers and a wide range of reduced frequency values. It was found that the behaviour of aerodynamic coefficients, vorticity fields and velocity fields are very sensitive to the reduced frequency.…”
Section: Dynamic Stallmentioning
confidence: 99%
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“…The laminar boundary layer on S809 airfoil blade was analyzed experimentally at zero attack angle, demonstrating that the separation bubble covers 19.6% of the chord length and a flow control technique is required to reduce the losses occurring due to separation, Abdulrahim et al [90]. An experimental study using an active flow control technique was carried out by Gharali and Johnson [91]. A three-bladed horizontal axis wind turbine rotor was tested in an open jet wind tunnel.…”
Section: Experimental Approach To Blade Design and Analysismentioning
confidence: 99%
“…An experimental study using an active flow control technique was carried out by Gharali and Johnson [91]. A three-bladed horizontal axis wind turbine rotor was tested in an open jet wind tunnel.…”
Section: Experimental Approach To Blade Design and Analysismentioning
confidence: 99%