Effects of torsional degree of freedom, geometric nonlinearity, and gravity on aeroelastic behavior of large-scale horizontal axis wind turbine blades under varying wind speed conditions

2014 ◽  
Vol 6 (2) ◽  
pp. 023126 ◽  
Author(s):  
Min-Soo Jeong ◽  
Myung-Chan Cha ◽  
Sang-Woo Kim ◽  
In Lee ◽  
Taeseong Kim
Author(s):  
Ohad Gur ◽  
Aviv Rosen

The optimal aerodynamic design of Horizontal Axis Wind Turbine (HAWT) is investigated. The Blade-element/Momentum model is used for the aerodynamic analysis. In the first part of the paper a simple design method is derived, where the turbine blade is optimized for operation at a specific wind speed. Results of this simple optimization are presented and discussed. Besides being optimized for operation at a specific wind speed, without considering operation at other wind speeds, the simple model is also limited in the choice of design goals (cost functions), design variables and constraints. In the second part of the paper a comprehensive design method that is based on a mixed numerical optimization strategy, is presented. This method can handle almost any combination of: design goal, design variables, and constraints. Results of this method are presented, compared with the results of the simple optimization, and discussed.


Author(s):  
Manoj Kumar Chaudhary ◽  
S Prakash

This paper aims to optimize and investigate the small horizontal axis wind turbine blades at low wind speed. The objective of this research work is to explain the design method based on BEM theory for 0.2 m blade rotors with constant, variable and linear chord with twisted blade geometry. MATLAB and Xfoil programs were used for BEM principles and wind turbines with SG6043 airfoil. A numerical and experimental study was carried out to examine the impact of rotor solidity from 0.057 to 0.207 and the number of blades from 3 to 7 in this research work. The experimental blades were developed by using the 3D printing additive manufacturing technique. The investigation of the rotors has been done in an open wind tunnel, at wind speed from 2 to 8 m/s. The initial investigation range included tip speed ratios from 2 to 8, and angle of attacks from 2 to 20°. Later on these parameters were varied in Matlab and Xfoil software optimization and investigation of the power coefficient, blade geometry, number of blades and blade pitch angle. It was found that the rotor solidity 0.055 to 0.085 displayed better performances.


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