Volume 12, Issue 1 pp. 457-458
Section 9
Free Access

An insight into the rotational stall delay

Horia Dumitrescu

Corresponding Author

Horia Dumitrescu

Institute of Statistics and Applied Mathematics, 13 Septembrie 13, sect. 5, 050711 Bucharest, Romania

Horia Dumitrescu, phone +4021 318 2433, fax +4021 318 2439

Cardos Vladimir, phone +4021 318 2433, fax +4021 318 2439

Florin Frunzulica, phone +4021 402 39 67, fax +4021 318 10 07

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Cardos Vladimir

Corresponding Author

Cardos Vladimir

Institute of Statistics and Applied Mathematics, 13 Septembrie 13, sect. 5, 050711 Bucharest, Romania

Horia Dumitrescu, phone +4021 318 2433, fax +4021 318 2439

Cardos Vladimir, phone +4021 318 2433, fax +4021 318 2439

Florin Frunzulica, phone +4021 402 39 67, fax +4021 318 10 07

Search for more papers by this author
Florin Frunzulica

Corresponding Author

Florin Frunzulica

Institute of Statistics and Applied Mathematics, 13 Septembrie 13, sect. 5, 050711 Bucharest, Romania

POLITEHNICA University of Bucharest, Faculty of Aerospace Engineering, Polizu 1–6, 011061, Bucharest, Romania

Horia Dumitrescu, phone +4021 318 2433, fax +4021 318 2439

Cardos Vladimir, phone +4021 318 2433, fax +4021 318 2439

Florin Frunzulica, phone +4021 402 39 67, fax +4021 318 10 07

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First published: 03 December 2012

Abstract

Blade element momentum (BEM) theory which is based on the two-dimensional (2D) aerodynamic properties of airfoil blade element is the most common computational engineering method for the prediction of loads and power curves of wind turbines. Although most BEM models yield acceptable results for high tip-speed ratios where the local angles of attack are small, no generally accepted model exists up to date that consistently predicts the loads and power in stall regime for stall-controlled turbines. Understanding of the stall delay phenomenon on wind turbines remains, to this day, incomplete. The lack of a conceptual model for the complex three-dimensional (3D) flow field on the rotor blade, where stall is begins, how it progresses and where stall is practically terminated, has hindered the finding of a unanimously accepted solution. The paper aims at giving a better understanding of the delayed stall events and a reasonably simple correction model that complements the 2D airfoil characteristics used to a BEM method. (© 2012 Wiley-VCH Verlag GmbH & Co. KGaA, Weinheim)

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