2013
DOI: 10.4324/9781849770408
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Aerodynamics of Wind Turbines, 2nd edition

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Cited by 180 publications
(254 citation statements)
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“…In practice this means that the actuator disc acts as a volume force onto the surrounding cells. It is argued by Vaal et al (2014) that, because this method explicitly solves the wake rather than relying on simplified relations, the method should be more robust than commonly used methods such as the Pitt-Peters model (Pitt and Peters, 1983) or the Stig Øye model (Hansen, 2008). Vaal et al (2014) present a number of investigations into the relative performance of the models; for this paper, the rotor plane induction is the most interesting to compare.…”
Section: Comparison Casesmentioning
confidence: 99%
See 1 more Smart Citation
“…In practice this means that the actuator disc acts as a volume force onto the surrounding cells. It is argued by Vaal et al (2014) that, because this method explicitly solves the wake rather than relying on simplified relations, the method should be more robust than commonly used methods such as the Pitt-Peters model (Pitt and Peters, 1983) or the Stig Øye model (Hansen, 2008). Vaal et al (2014) present a number of investigations into the relative performance of the models; for this paper, the rotor plane induction is the most interesting to compare.…”
Section: Comparison Casesmentioning
confidence: 99%
“…Tran et al (2014) also compared their results against lower-order simulations using the unsteady blade element momentum method. The Tran et al (2014) implementation of the unsteady blade element moment (UBEM) method was taken from Hansen (2008) with corrections for tip losses, wake unsteadiness and unsteady aerodynamics. This particular implementation took the platform motion into account by changing the relative inflow velocity.…”
Section: Comparison Casesmentioning
confidence: 99%
“…The geometrical dimensions of different scaled blades are proportional to the scale factor, denoted as R. Correspondingly, the structural and aerodynamic parameters are related to the scale factor, as shown in Table 2. The aerodynamic bending moment can be orthogonally divided into flap-wise moment M x and edge-wise moment M y [44]. Table 2.…”
Section: Upscaling Studies Of Sectional Bladesmentioning
confidence: 99%
“…This motion mainly affects the thrust force. Using the assumption of an ideal rotor it is possible to derive a simple one-dimensional model for estimating the thrust force, F , at tower top (Hansen, 2008) 5…”
Section: Integrated and Decoupled Dynamic Analysismentioning
confidence: 99%