Parametric Design Method and Performance Analysis of Double S-Shaped Nozzles

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/4694837/figures/4694837.fig.009a.svgz" name="4694837.fig.009a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Upper wall</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/4694837/figures/4694837.fig.009b.svgz" name="4694837.fig.009b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Lower wall</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/4694837/figures/4694837.fig.009c.svgz" name="4694837.fig.009c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Side wall</td></tr></table>

<div>Effects of offset ratios on wall pressure.</div>

International Journal of Aerospace Engineering

fig9

Figure 9

Figure 9: Parametric Design Method and Performance Analysis of Double S-Shaped Nozzles 