Effect of Plunging Oscillation on an Offshore Wind Turbine Blade Section
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Effect of Plunging Oscillation on an Offshore Wind Turbine Blade Section

Authors: F. Rasi Marzabadi

Abstract:

A series of experiments were carried out to study unsteady behavior of the flow field as well as the boundary layer of an airfoil oscillating in plunging motion in a subsonic wind tunnel. The measurements involved surface pressure distribution complimented with surface-mounted hot-films. The effect of leadingedge roughness that simulates surface irregularities on the wind turbine blades was also studied on variations of aerodynamic loads and boundary layer behavior.

Keywords: Boundary layer transition, plunging, reduced frequency, wind turbine.

Digital Object Identifier (DOI): doi.org/10.5281/zenodo.1331019

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References:


[1] Spera, D.A., "Wind Turbine Technology, Fundamental Concepts of Wind Turbine Engineering," ASME Press, USA, 1998, pp. 1-46.
[2] Bianchi, D.F., Battista, H.D., and Mantz, R.J., Wind Turbine Control Systems, Springer, Germany, 2007, pp. 8-30.
[3] Manwell, J.F., McGowan, J.G., and Rogers, A.L., Wind Energy Explained Theory, Design and Application, John Wiley and Sons Ltd, England, 2002, pp. 1-20.
[4] Tempel, V.D.J., "Design of Support Structures for offshore Wind Turbines," PhD Thesis, Delft University of Technology, Netherland, 2006, pp. 7-17.
[5] Jonkman, J.M. and Buhl, J., "Loads analysis of a floating offshore wind turbine using fully coupled simulation," National Renewable Energy Laboratory, PhD Thesis, NREL, USA, 2007, pp. 1-200.
[6] Leishman, J., "Challenges in modeling the unsteady aerodynamics of wind turbines," AIAA 2002-0037, 21st ASME Wind Energy Symposium and 40th AIAA Aerospace Sciences Meeting, Reno, NV, January 2002.
[7] Hansen, AC, Butterfield, CP, "Aerodynamics of Horizontal-Axis Wind Turbine," Annual Review of Fluid Mechanics, Vol. 25, 1993, pp.115- 149.
[8] McAllister, K.W., Carr, L.W. and McCroskey, W.J. "Dynamic stall experiments on the NACA 0012 Aerofoil," NASA TP-1100, January 1978.
[9] Ericsson, L.E., and Reding, J.P., "Shock-induced dynamic stall," Journal of Aircraft, Vol. 21, May 1984, pp 316-321.
[10] Carr, L.W. "Progress in analysis and prediction of dynamic stall," AIAA Journal, Vol. 25, 1988, 1, pp. 6-17.
[11] Fukushima, T. and Dadone, L.U. "Comparison of dynamic stall phenomena for pitching and vertical translation motions," NASA CR- 2793, July 1977.
[12] Rooij, RPJOM, Timmer, WA, "Roughness Sensitivity Considerations for Thick Rotor Blade Airfoils," Journal of Solar Energy Engineering, Vol. 125, 2003.
[13] Hu, Hui, Yang, Zifeng, and Igarashi, Hirofumi, "Aerodynamic Hysteresis of a Low-Reynolds-Number Airfoil," Journal of Aircraft, Vol. 44, No. 6, 2007, pp. 2083-2086.
[14] Barlow, J. B., Rae, W. H., and Pope, A., Low-Speed Wind Tunnel Testing, 3rd Edition, John Wiley & Sons, 1999.
[15] Soltani, MR and Rasi Marzabadi, F, "Effect of Plunging Amplitude on the Performance of a Wind Turbine Blade Section," The Aeronautical Journal, Vol. 111, No. 1123, 2007, pp. 571-587.
[16] Ericson, L.E., and Reding, J.P., "Unsteady Flow Concepts for Dynamic Stall Analysis," AIAA Journal of Aircraft, Vol.21, No. 8, Aug. 1984, pp. 601-606.
[17] Hodson, HP, and Howell, RJ, "Unsteady Flow: Its role in the Low Pressure Turbine," 9th International Symposium Unsteady Aerodynamics, Aeroacoustics and Aeroelasticity of Turbomachines, Lyon, 2000.
[18] Zhang, XF, Mahallati, A, and Sjolander, SA, "Hot-Film Measurements of Boundary Layer Transition, Separation and Reattachment on a Low Reynolds Numbers," AIAA 2002-3643, 38th AIAA/ASME/SAE/ASEE Joint Propulsion Conference & Exhibit, 2002.
[19] Carta, F. A., "A Comparison of the Pitching and Plunging Response of an Oscillating Airfoil," NASA CR-3172, 1979.
[20] Theodoresen, T., "General Theory of Aerodynamic Instability and the Mechanism of Flutter," NACA TR-496, 1935.