Computational Study on Effect of Synthetic Jet Design Parameters

<table>Instantaneous <i>Q</i> isosurfaces of Case <svg height="10.9125" id="M53" 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="M412 140l28 -9q0 -2 -35 -131h-373v23q112 112 161 170q59 70 92 127t33 115q0 63 -31 98t-86 35q-75 0 -137 -93l-22 20l57 81q55 59 135 59q69 0 118.5 -46.5t49.5 -122.5q0 -62 -29.5 -114t-102.5 -130l-141 -149h186q42 0 58.5 10.5t38.5 56.5z" id="x32"></path></g>
</svg> (high frequency case).</table>

International Journal of Aerospace Engineering

fig6

Figure 6

Figure 6: Computational Study on Effect of Synthetic Jet Design Parameters 