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Development of an icing simulation code for rotating wind turbines

journal contribution
posted on 2021-03-26, 10:53 authored by Chankyu Son, Taeseong Kim
This study aims to develop a three-dimensional icing simulation code named WISE (Wind turbine Icing Simulation code with performance Evaluation) integrated into OpenFOAM®. The freely available source code can contribute to icing simulations that require parallel computations. The rotational motion is explained by a Moving Reference Frame (MRF) in both aerodynamic and droplet fields. The thin water film theory is applied in the thermodynamic module. To verify WISE, ice accretion shapes on NREL Phase VI under rime and glaze icing conditions were considered. The ice accretion shapes obtained by WISE were compared against FENSAP-ICE and another numerical simulation without the MRF method for the droplet field. For the rime condition, the icing limits, maximum thickness, and its location are well predicted by WISE compared with FENSAP-ICE while the simulation without the MRF method overestimates the icing limits and maximum thickness. For the glaze condition, only WISE and FENSAP-ICE results are compared where the icing limits are slightly different. On the suction side, WISE accurately predicts the maximum thickness, ice growth direction, and icing limits. However, the thickness of ice on the pressure side is underestimated. It might be necessary to have a turbulence model that can predict the flow transition.

Funding

European Union’s Horizon 2020 research and innovation program under the Marie Sklodowska-Curie grant agreement no. 713683 (COFUNDfellowsDTU)

ADD (Agency for Defense Development) of Korea. (UD160053BD)

History

School

  • Mechanical, Electrical and Manufacturing Engineering

Published in

Journal of Wind Engineering and Industrial Aerodynamics

Volume

203

Publisher

Elsevier BV

Version

  • VoR (Version of Record)

Rights holder

© Elsevier

Publisher statement

This paper was accepted for publication in the journal Journal of Wind Engineering and Industrial Aerodynamics and the definitive published version is available at https://doi.org/10.1016/j.jweia.2020.104239.

Acceptance date

2020-05-09

Publication date

2020-06-10

Copyright date

2020

ISSN

0167-6105

eISSN

1872-8197

Language

  • en

Depositor

Prof Taeseong Kim. Deposit date: 22 March 2021

Article number

104239

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