Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap

<div class="floats-full-page floats-full-page-figure"><h2>Figure 9</h2><div class="floats-full-page-caption"><div>Static pressure distributions for different Reynolds numbers at AoA = 12° for the airfoil without and with GF.</div></div><div class="floats-full-page-content"><table class="figure-group"><tr class="fig-image"><td><object data="https://static-01.hindawi.com/articles/ijrm/volume-2015/628632/figures/628632.fig.009.svgz" name="628632.fig.009" type="image/svg+xml"></object></td></tr></table></div></div>

Figure 9 | Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap

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Figure 9: Effect of Reynolds Number on Aerodynamics of Airfoil with Gurney Flap

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Figure 9

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<p><em>International Journal of Rotating Machinery </em>publishes original research articles as well as review articles on all types of rotating machinery employing gas, vapor, particle, liquid, and their mixtures (including slurry) as the working substances.</p>


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