Wind energy represents nowadays a very important source of energy for many countries. It provides an efficient and effective solution to reduce fuel consumption as well as pollutant emissions. VAWTs (vertical axis wind turbines) were originally considered as very promising, before being superseded by the present, horizontal axis turbines. There is now a resurgence of interests for VAWTs, in particular Darrieus turbines. VAWTs like the H-rotor Darrieus turbine appear to be particularly promising for low wind speed conditions, but suffer from a low efficiency compared to horizontal axis turbines. Additionally, Darrieus turbines are not self-starting, which is a major drawback. The present paper introduces a new idea to improve the global performance of Darrieus rotors, relying on a slotted flap. Due to its low manufacturing costs and size, a two-bladed H-rotor with a radius of 2 meters was retained as a first application example. The blade airfoil relies on the S1046 profile, which was shown in previous studies to be superior under relevant operating conditions [1]. The solidity (Nc/R) of the rotor is kept at 0.25 for all the computations. In the first step a parametric geometry is created, where the end of the blade is converted into a slotted flap (with appropriate rounding). The main parameters are the distance between the main part of the blade and the flap (width of gap), the angle of the slot and the angle of the flap. In the second step a systematic analysis of the effect of those variables on the force and power coefficient is carried out using three-dimensional full factorial Design-of-Experiment with an in-house parameterization and optimization software. For each configuration, force and power coefficients are calculated for four different tip-speed ratios (including the value, where the S1046 profile without flap shows its maximal power coefficient). The evaluation of each configuration is performed using a commercial CFD software. The flow is assumed in this first study to be two-dimensional and unsteady. Turbulence intensities follow the relevant norms (DIN EN 61400). Finally the results are compared to each other and to the reference design (S1046 without flap) and conclusions are given regarding power coefficient and flap load.
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ASME Turbo Expo 2014: Turbine Technical Conference and Exposition
June 16–20, 2014
Düsseldorf, Germany
Conference Sponsors:
- International Gas Turbine Institute
ISBN:
978-0-7918-4566-0
PROCEEDINGS PAPER
Analysis of the Effect of a Slotted Flap Mechanism on the Performance of an H-Darrieus Turbine Using CFD
László Daróczy,
László Daróczy
University of Magdeburg “Otto von Guericke”, Magdeburg, Germany
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Mohamed H. Mohamed,
Mohamed H. Mohamed
Helwan University, Cairo, Egypt
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Gábor Janiga,
Gábor Janiga
University of Magdeburg “Otto von Guericke”, Magdeburg, Germany
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Dominique Thévenin
Dominique Thévenin
University of Magdeburg “Otto von Guericke”, Magdeburg, Germany
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László Daróczy
University of Magdeburg “Otto von Guericke”, Magdeburg, Germany
Mohamed H. Mohamed
Helwan University, Cairo, Egypt
Gábor Janiga
University of Magdeburg “Otto von Guericke”, Magdeburg, Germany
Dominique Thévenin
University of Magdeburg “Otto von Guericke”, Magdeburg, Germany
Paper No:
GT2014-25250, V03BT46A003; 10 pages
Published Online:
September 18, 2014
Citation
Daróczy, L, Mohamed, MH, Janiga, G, & Thévenin, D. "Analysis of the Effect of a Slotted Flap Mechanism on the Performance of an H-Darrieus Turbine Using CFD." Proceedings of the ASME Turbo Expo 2014: Turbine Technical Conference and Exposition. Volume 3B: Oil and Gas Applications; Organic Rankine Cycle Power Systems; Supercritical CO2 Power Cycles; Wind Energy. Düsseldorf, Germany. June 16–20, 2014. V03BT46A003. ASME. https://doi.org/10.1115/GT2014-25250
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