Experimental investigations of airfoil surface flow of a horizontal axis wind turbine with LDV measurements

Energy ◽  
2020 ◽  
Vol 191 ◽  
pp. 116558
Author(s):  
Qing’an Li ◽  
Jianzhong Xu ◽  
Yasunari Kamada ◽  
Maeda Takao ◽  
Shogo Nishimura ◽  
...  
Energy ◽  
2019 ◽  
Vol 183 ◽  
pp. 341-357 ◽  
Author(s):  
Qing'an Li ◽  
Jianzhong Xu ◽  
Takao Maeda ◽  
Yasunari Kamada ◽  
Shogo Nishimura ◽  
...  

Author(s):  
Manoj Kumar Chaudhary ◽  
◽  
S. Prakash ◽  

In this research work, the investigation and optimization of small horizontal axis wind turbine blade at low wind speed is pursued. The experimental blades were developed using the 3D printing additive manufacturing technique. The airfoils E210, NACA2412, S1223, SG6043, E216, NACA4415, SD7080, SD7033, S1210 and MAF were tested at the wind speed of 2-6 m/s. The airfoils and optimum blade geometry were investigated with the aid of the Xfoil software at Reynolds number of 100,000. The initial investigation range included tip speed ratios from 3 to 10, solidity from 0.0431 – 0.1181 and angle of attacks from 2o to 20o. Later on these parameters were varied in MATLAB and Xfoil software for optimization and investigation of the power coefficient, lift coefficient, drag coefficient and lift to drag ratio. The cut-in wind speed of the rotors was 2 and 2.5 m/s with the winglet-equipped blades and without winglets. It was found that the E210, SG6043, E216 NACA4415 and MAF airfoil displayed better performance than the NACA 2412, S1223, SD7080, S1210 & SD7003 for the geometry optimized for the operating conditions and manufacturing method described.


2017 ◽  
Vol 140 (2) ◽  
Author(s):  
M. A. Ben Hassena ◽  
F. Najar ◽  
S. Choura ◽  
F. H. Ghorbel

In this paper, we propose a new coupled dynamical model of a horizontal axis wind turbine (HAWT). The proposed model takes into consideration the dynamic coupling of the flexible tower with both bending and torsion of the flexible blades. This model also accounts for the dynamics of an additional point mass located in one of the blades to simulate a crack. In addition, a finite element model (FEM) analysis along with an experimental study is conducted in this research to validate the modal analysis of a HAWT prototype. Data from the analytical, numerical, and experimental investigations were collected and showed comparable findings. Using the analytical model, the modal analysis and the steady-state response of the HAWT prototype are performed for two configurations: with and without a crack. In this paper, we also propose a new model-based technique for the detection of cracks in the HAWT.


2010 ◽  
Vol 2010.2 (0) ◽  
pp. 121-122
Author(s):  
Yasunari KAMADA ◽  
Takao MAEDA ◽  
Junsuke MURATA ◽  
Satoshi MATSUDA ◽  
Thibault MATHIEU ◽  
...  

2002 ◽  
Vol 124 (4) ◽  
pp. 335-344 ◽  
Author(s):  
E. A. Mayda ◽  
C. P. van Dam

The effect of laminar separation bubbles on the surface pressure distribution and aerodynamic force characteristics of a horizontal axis wind turbine airfoil is studied numerically. The NREL S809 airfoil for stall-controlled horizontal-axis wind turbines is analyzed at a chord Reynolds number of 1.0×106. For all flow conditions involving laminar separation in the present study, bubble-induced vortex shedding is observed. This flow phenomenon causes significant oscillations in the airfoil surface pressures and, hence, in the airfoil-generated aerodynamic forces. The computed time-averaged pressures compare favorably with wind-tunnel measurements.


Author(s):  
Essam E. Khalil ◽  
Gamal E. ElHarriri ◽  
Eslam E. AbdelGhany ◽  
Moemen E. Farghaly

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