This paper presents comparative study different airfoils from NACA and NREL Airfoil families focusing on their suitability for small wind turbine. In this point of view, four criteria of comparison have been taken into account. The criteria are: maximum glide ratio at lower and higher Reynolds number, difference between angle of attack between lower and higher Reynolds number and percentage deviation of maximum glide ratio from stall point. XFOIL analysis with the help of Qblade software results in data necessary for comparing two families of airfoil which finally show that NACA airfoils have better average performance criteria whereas NREL airfoils have better stability criteria
Selection of appropriate airfoil is very important for improved aerodynamic performance of a smaller...
Selection of appropriate airfoil is very important for improved aerodynamic performance of a smaller...
Summarization: The present study introduces a low Reynolds number (Re) airfoil family for the entire...
For better designing of an airfoil, the aerodynamic characteristics of the airfoil need to be invest...
Small wind turbine power generation systems have the potential to meet the electricity demand of the...
It is found that the usage of conventional aircraft airfoil sections is not the proper choice for wi...
Assessment of drag coefficient frequently requires experiment in wind tunnel and experimenting with ...
In contrast to large horizontal axis wind turbines (HAWTs) that are located in areas dictated by opt...
In this study aerodynamic performance of the different wind turbine airfoils that can work efficient...
A detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid...
In this study, we have focused on commonly used 14 different small wind turbine airfoils (A18, BW3, ...
In this study aerodynamic performance of the different wind turbine airfoils that can work efficient...
A successful blade design must satisfy some criterions which might be in conflict with maximizing an...
The horizontal axis wind turbine (HAWT) design with low wind speed requires blade geometry selection...
The horizontal axis wind turbine (HAWT) design with low wind speed requires blade geometry selection...
Selection of appropriate airfoil is very important for improved aerodynamic performance of a smaller...
Selection of appropriate airfoil is very important for improved aerodynamic performance of a smaller...
Summarization: The present study introduces a low Reynolds number (Re) airfoil family for the entire...
For better designing of an airfoil, the aerodynamic characteristics of the airfoil need to be invest...
Small wind turbine power generation systems have the potential to meet the electricity demand of the...
It is found that the usage of conventional aircraft airfoil sections is not the proper choice for wi...
Assessment of drag coefficient frequently requires experiment in wind tunnel and experimenting with ...
In contrast to large horizontal axis wind turbines (HAWTs) that are located in areas dictated by opt...
In this study aerodynamic performance of the different wind turbine airfoils that can work efficient...
A detailed numerical investigation of the aerodynamic performance on the five airfoils namely Mid...
In this study, we have focused on commonly used 14 different small wind turbine airfoils (A18, BW3, ...
In this study aerodynamic performance of the different wind turbine airfoils that can work efficient...
A successful blade design must satisfy some criterions which might be in conflict with maximizing an...
The horizontal axis wind turbine (HAWT) design with low wind speed requires blade geometry selection...
The horizontal axis wind turbine (HAWT) design with low wind speed requires blade geometry selection...
Selection of appropriate airfoil is very important for improved aerodynamic performance of a smaller...
Selection of appropriate airfoil is very important for improved aerodynamic performance of a smaller...
Summarization: The present study introduces a low Reynolds number (Re) airfoil family for the entire...