Computational Study on Effect of Synthetic Jet Design Parameters

<table>Instantaneous <i>Q</i> isosurfaces of Case <svg height="10.9125" id="M49" style="vertical-align:-0.0pt" version="1.1" viewbox="0 0 8.2875004 10.9125" width="8.2875004" xmlns="http://www.w3.org/2000/svg" xmlns:xlink="http://www.w3.org/1999/xlink">
<g transform="matrix(.017,-0,0,-.017,.062,10.862)"><path d="M384 0h-275v27q67 5 81.5 18.5t14.5 68.5v385q0 38 -7.5 47.5t-40.5 10.5l-48 2v24q85 15 178 52v-521q0 -55 14.5 -68.5t82.5 -18.5v-27z" id="x31"></path></g>
</svg> (low frequency case). (Isosurfaces are colored with <i>y</i>-vorticity).</table>

International Journal of Aerospace Engineering

fig5

Figure 5

Figure 5: Computational Study on Effect of Synthetic Jet Design Parameters 