Articles | Volume 8, issue 2
https://doi.org/10.5194/wes-8-211-2023
https://doi.org/10.5194/wes-8-211-2023
Research article
 | 
20 Feb 2023
Research article |  | 20 Feb 2023

Progress in the validation of rotor aerodynamic codes using field data

Koen Boorsma, Gerard Schepers, Helge Aagard Madsen, Georg Pirrung, Niels Sørensen, Galih Bangga, Manfred Imiela, Christian Grinderslev, Alexander Meyer Forsting, Wen Zhong Shen, Alessandro Croce, Stefano Cacciola, Alois Peter Schaffarczyk, Brandon Lobo, Frederic Blondel, Philippe Gilbert, Ronan Boisard, Leo Höning, Luca Greco, Claudio Testa, Emmanuel Branlard, Jason Jonkman, and Ganesh Vijayakumar

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Cited articles

Bak, C. and Fuglsang, P.: A Method for Deriving 3D Airfoil Characteristics for a Wind Turbine, in: 42th AIAA Aerospacce Sciences Meeting and Exhibit, 5–8 January 2004, Reno, Nevada, AIAA-2004-0666, 2004. a, b
Bak, C., Madsen, H., Paulsen, U. S., Gaunaa, M., Sørensen, N., Fuglsang, P., Romblad, J., Olsen, N., Enevoldsen, P., Laursen, J., and Jensen, L.: DAN-AERO MW: Detailed aerodynamic measurements on a full scale MW wind turbine, in: European Wind Energy Conference and Exhibition 2010, Ewec 2010, 2, 20–23 April 2010, Warsaw, Poland, 792–836, 2010. a, b, c
Bak, C., Madsen, H., Troldborg, N., Gaunaa, M., Skrzypinski, W., Fischer, A., Paulsen, U., Møller, R., Hansen, P., Rasmussen, M., and Fuglsang, P.: DANAERO MW: Instrumentation of the NM80 turbine and meteorology mast at Tjæreborg, Report-I-0083, DTU Wind Energy, https://orbit.dtu.dk/ (last access: 13 November 2017), 2013. a
Bangga, G.: Comparison of Blade Element Method and CFD Simulations of a 10 MW Wind Turbine, Fluids, 3, 73, https://doi.org/10.3390/fluids3040073, 2018. a
Bauchau, O., Bottasso, C., and Nikishkov, Y.: Modeling rotorcraft dynamics with finite element multibody procedures, Math. Comput. Model., 33, 1113–1137, https://doi.org/10.1016/S0895-7177(00)00303-4, 2001. a
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Within the framework of the fourth phase of the International Energy Agency's (IEA) Wind Task 29, a large comparison exercise between measurements and aeroelastic simulations has been carried out. Results were obtained from more than 19 simulation tools of various fidelity, originating from 12 institutes and compared to state-of-the-art field measurements. The result is a unique insight into the current status and accuracy of rotor aerodynamic modeling.
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