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.007a.svgz" name="4694837.fig.007a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Plume boundary grid</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/4694837/figures/4694837.fig.007b.svgz" name="4694837.fig.007b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Nozzle wall grid</td></tr><tr class="fig-image" id="c"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/4694837/figures/4694837.fig.007c.svgz" name="4694837.fig.007c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Pressure</td></tr><tr class="fig-image" id="d"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2019/4694837/figures/4694837.fig.007d.svgz" name="4694837.fig.007d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>Mach number</td></tr></table>

<div>Schematic computational grids and grid independency.</div>

International Journal of Aerospace Engineering

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Figure 7

Figure 7: Parametric Design Method and Performance Analysis of Double S-Shaped Nozzles 