Volume 6B: Energy 2014
DOI: 10.1115/imece2014-36082
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Enhancement of Free Vortex Filament Method for Aerodynamic Loads on Rotor Blades

Abstract: The aerodynamics of a wind turbine is governed by the flow around the rotor

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Cited by 13 publications
(13 citation statements)
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“…The helix is treated as a vortex filament that generates an induced velocity field, u ind;k . This filament is discretized into small straight-line vortex segments having constant circulation Γ, and the induced velocity at a given point is evaluated numerically by means of the Biot-Savart law [45,49] applied to each segment [50]:…”
Section: Improved Rans-informed Method: Novel Tip Vortex Modelmentioning
confidence: 99%
See 1 more Smart Citation
“…The helix is treated as a vortex filament that generates an induced velocity field, u ind;k . This filament is discretized into small straight-line vortex segments having constant circulation Γ, and the induced velocity at a given point is evaluated numerically by means of the Biot-Savart law [45,49] applied to each segment [50]:…”
Section: Improved Rans-informed Method: Novel Tip Vortex Modelmentioning
confidence: 99%
“…In Eq. (15), r A and r B are the vectors connecting the segment extrema with the evaluation point (see [50]). A form for the correction factor K v must be defined to model the effect of a viscous core with finite radial extent.…”
Section: Improved Rans-informed Method: Novel Tip Vortex Modelmentioning
confidence: 99%
“…The lift calculation could be executed employing a) Fourier method or b) simplified method with different approaches. A vortex filament method for aerodynamic load calculations have been developed on rotor blades (Abedi, 2013).…”
Section: The Extended Lifting Line Theory For 3-d Wind Turbine Blade mentioning
confidence: 99%
“…In particular, linear inflow models are known to under-estimate the harmonic content of the forces. Computational Fluid Dynamics (CFD) is usually used to solve the aerodynamic field of every single blade, while the induced velocity is computed through potential methods, such as the prescribed or free-wake method (24) . However, we strive to avoid computationally intense tasks, such those arising from CFD simulations, because we need to simulate several seconds of flight to validate the controllers.…”
Section: Numerical Modellingmentioning
confidence: 99%