Renewable Energy 2018
DOI: 10.4324/9781315793245-89
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Applied Aerodynamics of Wind Power Machines

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Cited by 78 publications
(41 citation statements)
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“…The BEM theory is, then, fully defined by applying the Glauert correction for high values of a (see Hansen 55 ) and can also be extended adding root losses, 31 estimating properly the aerodynamic coefficients, induction factors and angle of attack for each blade element. According to Burton et al, 31 Wilson and Lissaman 56 argue that the drag coefficient should not be included in the calculus of the normalized coefficients.…”
Section: Orcidmentioning
confidence: 99%
“…The BEM theory is, then, fully defined by applying the Glauert correction for high values of a (see Hansen 55 ) and can also be extended adding root losses, 31 estimating properly the aerodynamic coefficients, induction factors and angle of attack for each blade element. According to Burton et al, 31 Wilson and Lissaman 56 argue that the drag coefficient should not be included in the calculus of the normalized coefficients.…”
Section: Orcidmentioning
confidence: 99%
“…In this paper, the Vortex model is used to model the SBDWT because it is the most accurate model as mentioned earlier. In Reference 25, the torque of each SBDWT's blade is modeled and Equation (1) represents the mathematical model for the torque of each blade of wind turbine. Q=ρπcRV213cX2Ritalicsinθ2sin2θ where Q i , ρ , c , R , V ∞ , X , and θ represent blade torque, fluid density, blade chord, rotor radius, wind velocity, tip speed ratio and blade rotation angle, respectively. In the three blades SBDWT, the angle between the blades is 120°.…”
Section: Modelingthe Vawt and Its Faultsmentioning
confidence: 99%
“…As mentioned earlier, the SBDWT is equipped with a pitch angle controller to overcome the starting torque. In Reference 25 the relationship between tip speed ratio and the pitch angle was mentioned. Equation (4) represents this relationship for the three blades SBDWT. X=1italictanϕ+3c2R where ϕ = α + γ , which α and γ represent the initial pitch angle and added or subtracted angle to pitch angle in pitch angle control, respectively.…”
Section: Modelingthe Vawt and Its Faultsmentioning
confidence: 99%
“…The mathematical model of the horizontal-axis wind turbine considered here is based on a stream tube discretization, which relies on momentum conservation in both the axial and tangential directions. The airfoil aerodynamic characteristics, the lift ( C L ) and drag ( C D ) coefficients, can be found in Wilson and Lissaman (1974). The thrust and torque acting on a blade element d r , at a distance r from the center of the rotor, are given by…”
Section: Mathematical Model Of the Horizontal-axis Wind Turbinementioning
confidence: 99%
“…The momentum models approximate the wind turbine effects using actuator surfaces and subdivide the flow domain in many stream tubes (see e.g. Islam et al, 2008; Torresi et al, 2013, 2016; Wilson and Lissaman, 1974). These models appear to be more suitable to describe the wind turbine dynamics for control applications.…”
Section: Introductionmentioning
confidence: 99%