Development and Validation of the IAG Dynamic Stall Model in State-Space Representation for Wind Turbine Airfoils

Author:

Bangga Galih1ORCID,Parkinson Steven1,Collier William1

Affiliation:

1. DNV Services UK Limited, One Linear Park, Avon Street, Temple Quay, Bristol BS2 0PS, UK

Abstract

Considering the dynamic stall effects in engineering calculations is essential for correcting the aerodynamic loads acting on wind turbines, both during power production and stand-still cases, and impacts significantly the turbine aeroelastic stability. The employed dynamic stall model needs to be accurate and robust for a wide range of airfoils and range of angle of attack. The present studies are intended to demonstrate the performance of a recently implemented “IAG dynamic stall” model in a wind turbine design tool Bladed. The model is transformed from the indicial type of formulation into a state-space representation. The new model is validated against measurement data and other dynamic stall models in Bladed for various flow conditions and airfoils. It is demonstrated that the new model is able to reproduce the measured dynamic polar accurately without airfoil specific parameter calibration and has a superior performance compared to the incompressible Beddoes–Leishman model and the Øye model in Bladed.

Funder

DNV research project

Publisher

MDPI AG

Subject

Energy (miscellaneous),Energy Engineering and Power Technology,Renewable Energy, Sustainability and the Environment,Electrical and Electronic Engineering,Control and Optimization,Engineering (miscellaneous),Building and Construction

Reference33 articles.

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4. McAlister, K.W., Carr, L.W., and McCroskey, W.J. (1978). Dynamic Stall Experiments on the NACA 0012 Airfoil, National Aeronautics and Space Administration. Technical Report, NASA Technical Paper 1100.

5. Ramsay, R., Hoffman, M., and Gregorek, G. (1996). Effects of Grit Roughness and Pitch Oscillations on the S801 Airfoil, National Renewable Energy Lab.. Technical Report.

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