2013
DOI: 10.1002/we.1606
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Laminar‐turbulent flow simulation for wind turbine profiles using the γ– transition model

Abstract: The accurate prediction of the laminar‐turbulence transition process is fundamental in predicting the aerodynamic performance of wind turbine profiles. Fully turbulent flow simulations have been shown to over‐predict the aerodynamic performance and thereby negatively impacting the design of airfoils in flow regimes where the possible presence of laminar flow could be exploited to improve the performance of wind turbine rotors. Correlation‐based transition modelling offers a fully computational fluid dynamics c… Show more

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Cited by 31 publications
(18 citation statements)
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“…Several researchers noted that a cause of the premature transition onset prediction was due to the function within the model that compared the strain-rate Reynolds number to the criteria for transition onset. 37 As discussed the model does not actually compute the momentum thickness of the boundary layer, but rather use the relationship between the maximal value of the strain rate Reynolds number and a calibrated constant. (see Eq.…”
Section: A Modifications To Onset Criteria For Langtry-menter Modelmentioning
confidence: 99%
“…Several researchers noted that a cause of the premature transition onset prediction was due to the function within the model that compared the strain-rate Reynolds number to the criteria for transition onset. 37 As discussed the model does not actually compute the momentum thickness of the boundary layer, but rather use the relationship between the maximal value of the strain rate Reynolds number and a calibrated constant. (see Eq.…”
Section: A Modifications To Onset Criteria For Langtry-menter Modelmentioning
confidence: 99%
“…In the original model the value 2.2 is selected to achieve a F onset1 equal to one within a Blasius boundary layer and this effect is taken into account through the correlation for the critical momentum-thickness Reynolds number presented in equation (3). However, previous works 14,19 for the γ-Re θ model observed the necessity to re-scale C onset1 at high Reynolds numbers.…”
Section: The γ−Equation Transition Modelmentioning
confidence: 91%
“…An example of such a study is presented in [18]. This section aims at evaluating the grid dimensions necessary to achieve mesh independence of the aerodynamic coefficients.…”
Section: Grid Convergence Studymentioning
confidence: 99%