Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coandă Jet

<table>Typical <svg height="19.674999" id="M14" style="vertical-align:-3.56265pt" version="1.1" viewbox="0 0 18.700001 19.674999" width="18.700001" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg> values in the turbulent boundary layer and velocity profiles in wall units for subsonic flow over flat plate, <svg height="12.5" id="M15" style="vertical-align:-0.1638pt" version="1.1" viewbox="0 0 58.212502 12.5" width="58.212502" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
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</svg>, medium grid; nozzle pressure ratio = 1.4. (Source: Menter [<a href="/journals/jre/2013/839319/#B23">23</a>], Salim and Cheah [<a href="/journals/jre/2013/839319/#B51">45</a>], and Economon and Milholen II [<a href="/journals/jre/2013/839319/#B52">46</a>]).</table>

Journal of Renewable Energy

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Figure 2

Figure 2: Computational Study on the Aerodynamic Performance of Wind Turbine Airfoil Fitted with Coandă Jet 