1992
DOI: 10.1016/0167-6105(92)90533-g
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Computational methods for the performance prediction of HAWTs

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Cited by 15 publications
(5 citation statements)
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“…However, the prescription of the wake structure leaves open some questions about how the wake will expand, the local pitch angle and what will be the consequences on its dynamics, while there is little doubt that the flow at the rotor will be correctly estimated. If the wake is expanding but its shape is still prescribed, no analytical solution is yet been found, and numerical models have been developed by using lifting-line methods 10 or vortex-lattice methods to predict the wake 11,12 often combined with panel methods to replicate the blade presence. The method of acceleration potential, where the rotor is treated as a weak perturbation to the incoming flow, allows the determination of simple asymptotic relationships and is a valid alternative to these vortex methods (VMs).…”
Section: Introductionmentioning
confidence: 99%
“…However, the prescription of the wake structure leaves open some questions about how the wake will expand, the local pitch angle and what will be the consequences on its dynamics, while there is little doubt that the flow at the rotor will be correctly estimated. If the wake is expanding but its shape is still prescribed, no analytical solution is yet been found, and numerical models have been developed by using lifting-line methods 10 or vortex-lattice methods to predict the wake 11,12 often combined with panel methods to replicate the blade presence. The method of acceleration potential, where the rotor is treated as a weak perturbation to the incoming flow, allows the determination of simple asymptotic relationships and is a valid alternative to these vortex methods (VMs).…”
Section: Introductionmentioning
confidence: 99%
“…Duquette and Visser [11] examined blade number and the solidity effect on the performance of HAWT with different theories such as BEMT, rigid wake mothod (RWM) according to Kotb [12] and expanding wake model (EWM) based on Gould and fiddes [13].…”
Section: Introductionmentioning
confidence: 99%
“…Prescribed wake modelling has for many years been seen as an alternative to more intensive free wake methods in providing aerodynamic performance estimates for helicopter rotors. This approach has also been applied to both HAWTs and VAWTs using both lifting line and lifting surface formulations [8][9][10][11]. The prescribed wake model can yield results of comparable accuracy to a free wake model if the wake is correctly prescribed, while requiring only a fraction of the computational power.…”
Section: Introductionmentioning
confidence: 99%