Please use this identifier to cite or link to this item: http://hdl.handle.net/11455/2818
標題: 動態失速模型在Double Multiple-Streamtubes模型之應用與探討
Investigation of Dynamic Stall Models on Double Multiple-Streamtubes Model Application
作者: 黃信豪
Huang, Sin-Hun
關鍵字: 垂直軸風力發電機;VAWT;動態失速;Double Multiple-Streamtubes;Dynamic Stall;Double Multiple-Streamtubes
出版社: 機械工程學系所
引用: [1] D. E. Berg, P. C. Klimas, and W. A. Stephenson, "Aerodynamic design and initial performance measurements for the SANDIA 34-metre diameter vertical-axis wind turbine," Wind Energy, vol. 1, pp. 14-17, 1989. [2] P. Lissaman, "Low-Reynolds-number airfoils," Annual Review of Fluid Mechanics, vol. 15, pp. 223-239, 1983. [3] P. Deglaire, Analytical Aerodynamic Simulation Tools for Vertical Axis Wind Turbines: Acta Universitatis Upsaliensis, 2010. [4] P. Wernert, W. Geissler, M. Raffel, and J. Kompenhans, "Experimental and numerical investigations of dynamic stall on a pitching airfoil," AIAA journal, vol. 34, pp. 982-989, 1996. [5] N. Fujisawa and M. Takeuchi, "Flow visualization and PIV measurement of flow field around a Darrieus rotor in dynamic stall," J Vis, vol. 1, pp. 379-386, 1999. [6] J. Leishman, "Dynamic stall experiments on the NACA 23012 aerofoil," Experiments in fluids, vol. 9, pp. 49-58, 1990. [7] M. Raffel, J. Kompenhans, and P. Wernert, "Investigation of the unsteady flow velocity field above an airfoil pitching under deep dynamic stall conditions," Experiments in fluids, vol. 19, pp. 103-111, 1995. [8] C. Simao Ferreira, G. van Kuik, G. van Bussel, and F. Scarano, "Visualization by PIV of dynamic stall on a vertical axis wind turbine," Experiments in fluids, vol. 46, pp. 97-108, 2009. [9] W. McCroskey, "Unsteady airfoils," Annual Review of Fluid Mechanics, vol. 14, pp. 285-311, 1982. [10] L. Jesch and D. Walton, "Reynolds number effects on the aerodynamic performance of a vertical axis wind turbine," 1980, pp. 323-332. [11] P. Fraunie, C. Beguier, I. Paraschivoiu, and G. Brochier, "Water channel experiments of dynamic stall on darrieus wind turbine blades," Journal of Propulsion and Power, vol. 2, pp. 445-449, 1986. [12] L. CARR, "Progress in analysis and prediction of dynamic stall," Journal of Aircraft, vol. 25, pp. 6-17, 1988. [13] K. F. Tchon and I. Paraschivoiu, "Navier-Stokes simulation of the flow around an airfoil in Darrieus motion," Journal of Fluids Engineering;(United States), vol. 116, 1994. [14] R. Templin, "Aerodynamic performance theory for the NRC vertical-axis wind turbine," NASA STI/Recon Technical Report N, vol. 76, p. 16618, 1974. [15] J. Strickland, "A performance prediction model for the Darrieus turbine," 1977, p. 3. [16] I. Paraschivoiu, "Double-multiple streamtube model for Darrieus in turbines," 1981, pp. 19-25. [17] B. Blackwell and R. Sheldahl, "Selected wind tunnel test results for the Darrieus wind turbine," Journal of Energy, vol. 1, pp. 382-386, 1977. [18] B. F. Blackwell, R. E. Sheldahl, and L. V. Feltz, "Wind tunnel performance data for the Darrieus wind turbine with NACA 0012 blades," Sandia Labs., Albuquerque, N. Mex.(USA)1976. [19] P. C. Klimas and R. E. Sheldahl, "Four aerodynamic prediction schemes for vertical-axis wind turbines: a compendium," Sandia Laboratories. Albuquerque, NM, 1978. [20] M. H. Worstell, U. S. D. o. Energy, S. Laboratories, and S. L. A. E. P. Division, Aerodynamic performance of the 17-metre-diameter Darrieus wind turbine: Department of Energy, Sandia Laboratories, 1979. [21] J. H. Strickland, B. Webster, and T. Nguyen, "Vortex model of the Darrieus turbine: An analytical and experimental study," NASA STI/Recon Technical Report N, vol. 80, p. 25887, 1980. [22] A. Allet and I. Paraschivoiu, "Viscous Flow and Dynamic Stall Effects on Vertical-Axis Wind Turbines," International Journal of Rotating Machinery, vol. 2, pp. 1-14, 1995. [23] M. Islam, D. S. K. Ting, and A. Fartaj, "Aerodynamic models for Darrieus-type straight-bladed vertical axis wind turbines," Renewable and Sustainable Energy Reviews, vol. 12, pp. 1087-1109, 2008. [24] I. Paraschivoiu, Wind turbine design: with emphasis on Darrieus concept: Presses inter Polytechnique, 2002. [25] H. Beri, "Double Multiple Streamtube Model and Numerical Analysis of Vertical Axis Wind Turbine," Energy and Power Engineering, vol. 03, pp. 262-270, 2011. [26] R. E. Sheldahl and P. C. Klimas, "Aerodynamic characteristics of seven symmetrical airfoil sections through 180-degree angle of attack for use in aerodynamic analysis of vertical axis wind turbines," Sandia National Labs., Albuquerque, NM (USA)1981. [27] M. H. Hansen, M. Gaunaa, and H. A. Madsen, "A Beddoes-Leishman type dynamic stall model in state-space and indicial formulations," Riso-r-1354 (en), Riso National Laboratory, Roskilde, Denmark, 2004. [28] T. Thbodohsbn, "General theory of aerodynamic instability and the mechanism of flutter," 1935. [29] C. Tran and D. Petot, "Semi-empirical model for the dynamic stall of airfoils in view of the application to the calculation of responses of a helicopter blade in forward flight," 1980. [30] J. W. Larsen, S. R. K. Nielsen, and S. Krenk, "Dynamic stall model for wind turbine airfoils," Journal of Fluids and Structures, vol. 23, pp. 959-982, 2007. [31] S. Wang, D. B. Ingham, L. Ma, M. Pourkashanian, and Z. Tao, "Numerical investigations on dynamic stall of low Reynolds number flow around oscillating airfoils," Computers & Fluids, vol. 39, pp. 1529-1541, 2010. [32] O. Guerri, A. Sakout, and K. Bouhadef, "Simulations of the fluid flow around a rotating vertical axis wind turbine," Wind Engineering, vol. 31, pp. 149-163, 2007.
摘要: 
本研究以CFD套裝軟體與DMST模型分析H-rotor形式之垂直軸風機的氣動力,將不同的動態失速模型(Boeing–Vertol模型、ONERA模型與Risφ模型)套用於DMST模型中,比對DMST模型的氣動力分析結果與CFD模擬結果。在風速為12 m/s,尖端速度比為0.5~3,DMST模型引用Boeing–Vertol模型分析氣動力,其分析結果與CFD模擬結果相近;Risφ模型分析中,先利用MATLAB對Risφ模型參數進行最佳化,再套入DMST模型中,其分析結果趨近於CFD的模擬結果,在ONERA模型分析中,與Risφ模型一樣,使用最佳化的方式得到模型參數,再套入DMST模型中,其分析結果沒辦法有效重現CFD的模擬結果。
URI: http://hdl.handle.net/11455/2818
其他識別: U0005-2607201221060600
Appears in Collections:機械工程學系所

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