دانلود Blade Design and Performance Analysis of Wind Turbine

ترجمه مقاله Blade Design and Performance Analysis of Wind Turbine
قیمت : 230,000 ریال
شناسه محصول : 2009083
نویسنده/ناشر/نام مجله : International Journal of ChemTech Research
سال انتشار: 2013
تعداد صفحات انگليسي : 8
نوع فایل های ضمیمه : Pdf+Word
حجم فایل : 915 Kb
کلمه عبور همه فایلها : www.daneshgahi.com
عنوان انگليسي : Blade Design and Performance Analysis of Wind Turbine

چکیده

Abstract

This paper reviews the design optimization of wind turbine blades through investigating the design methods and analyzing the performance of the blades. The current research work in this area include wind turbine blade geometric design and optimization, aerodynamics analysis, wind turbine blade structural design and dynamics analysis. Blade geometric design addresses the design parameters, including airfoils and their aerodynamic coefficients, attack angles, design tip speed ratio, design and/or rated wind speed, rotor diameter, blade aerodynamic shape with chord length and twist distributions, so that the blade achieves an optimum power performance. The geometry of the blade is an aerodynamic shape with nonlinear chord and twist distribution, which can be obtained based on the BEM theory with respect to given aerofoil with known aerodynamic coefficients. In terms of blade aerodynamics analysis, there are four types of aerodynamic models which can be used to predict the aerodynamic performance of blades, including blade element momentum (BEM) model, lifting panel and vortex model, actuator line model, and computational fluid dynamics (CFD) model. Among the four, computational fluid dynamics (CFD) model has been used to calculate the aerodynamic effect on the blade airfoil. Critical Reynolds number and constant wind speed has been considered during analysis under different turbulence models Viz, spallart-almaras, k-epsilon, invicid flow. During investigation it is observed that only k-epsilon showed efficient results than others and 14 degree angle of attack (AOA) is the optimum value at which there is much lift coefficient and minimum drag.

Keywords: Angle of attack α aerodynamic coefficients cl & cd blade aerofoil
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