Abstract
The state of the art engineering dynamic inflow models of Pitt-Peters, Øye and ECN have been used to correct Blade Element Momentum theory for unsteady load prediction of a wind turbine for two decades. However, their accuracy is unknown. This paper is to benchmark the performance of these engineering models by experimental and numerical methods. The experimental load and flow measurements of an unsteady actuator disc were performed in the Open Jet Facility at Delft University of Technology. The unsteady load was generated by a ramp-type variation of porosity of the disc. A Reynolds Averaged Navier-Stokes (RANS) model, a Free Wake Vortex Ring (FWVR) model and a Vortex Tube Model (VTM) simulate the same transient load changes. The velocity field obtained from the experimental and numerical methods are compared with the engineering dynamic inflow models. Velocity comparison aft the disc between the experimental and numerical methods shows the numerical models of RANS and FWVR model are capable to predict the velocity transient behaviour during transient disc loading. Velocity comparison at the disc between the engineering models and the numerical methods further shows that the engineering models predict much faster velocity decay, which implies the need for more advanced or better tuned dynamic inflow models.
Highlights
IntroductionIntroduction and ObjectiveA wind turbine operates in a highly dynamic state. The currently most popular design theory of wind turbine — BEM, is based on the assumption of quasi-steady state
Introduction and ObjectiveA wind turbine operates in a highly dynamic state
Knight [14] has shown that the aerodynamic thrust of an actuator disc is insensitive to Reynolds number when it is larger than 150000 using tunnel test of three different types of discs
Summary
Introduction and ObjectiveA wind turbine operates in a highly dynamic state. The currently most popular design theory of wind turbine — BEM, is based on the assumption of quasi-steady state. The steady assumption made in BEM is at two levels, unsteady airfoil aerodynamics, and unsteady wake in the momentum theory. A CFD model was developed for unsteady rotor aerodynamics by Sørensen and Kock [4], the calculated blade flapping moment was in close agreement with experimental results for step blade pitch of 2MW Tjæreborg wind turbine. Good agreement with the latter experiment [3] for low loading case was achieved using BEM coupling with tuned time constants, which were tuned by solving RANS equations [5]
Talk to us
Join us for a 30 min session where you can share your feedback and ask us any queries you have
Disclaimer: All third-party content on this website/platform is and will remain the property of their respective owners and is provided on "as is" basis without any warranties, express or implied. Use of third-party content does not indicate any affiliation, sponsorship with or endorsement by them. Any references to third-party content is to identify the corresponding services and shall be considered fair use under The CopyrightLaw.