Wind energy production has been increasing steadily in the past decade. The majority of wind power is generated by horizontal axis wind turbines (HAWT). We investigate the modeling of the HAWT using the vortex panel method, which is an inviscid, steady, computationally inexpensive method. Pressure coefficient profiles, calculated by the vortex panel method, were compared to NREL phase VI wind turbine experiments under two different flow conditions. We show that if the flow is not separated over the blade, the vortex panel method can capture the pressure profile on the blade. Furthermore, the panel method has been extended to handle unsteady inviscid flows to investigate the effect of blade oscillations on the power generation, which is not known. The unsteady behavior is modeled by accounting for the time rate of change of circulation. Unsteady effects due to heaving and pitching motion were quantified for different blade oscillation frequencies. It is estimated that the mean thrust coefficient with heaving and pitching motion can be higher than the thrust generated without blade motion in some cases assuming that the flow does not separate.
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ASME 2014 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference
August 17–20, 2014
Buffalo, New York, USA
Conference Sponsors:
- Design Engineering Division
- Computers and Information in Engineering Division
ISBN:
978-0-7918-4628-5
PROCEEDINGS PAPER
NREL Phase VI Wind Turbine Modeling Using an Unsteady Panel Method
Eugene Grigoriev,
Eugene Grigoriev
State University of New York at Buffalo, Buffalo, NY
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Iman Borazjani
Iman Borazjani
State University of New York at Buffalo, Buffalo, NY
Search for other works by this author on:
Eugene Grigoriev
State University of New York at Buffalo, Buffalo, NY
Iman Borazjani
State University of New York at Buffalo, Buffalo, NY
Paper No:
DETC2014-34141, V01AT02A002; 10 pages
Published Online:
January 13, 2015
Citation
Grigoriev, E, & Borazjani, I. "NREL Phase VI Wind Turbine Modeling Using an Unsteady Panel Method." Proceedings of the ASME 2014 International Design Engineering Technical Conferences and Computers and Information in Engineering Conference. Volume 1A: 34th Computers and Information in Engineering Conference. Buffalo, New York, USA. August 17–20, 2014. V01AT02A002. ASME. https://doi.org/10.1115/DETC2014-34141
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