Study on Size Distribution and Flow Characteristics of Condensed Products in Solid Rocket Motor

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/5481436/figures/5481436.fig.005a.svgz" name="5481436.fig.005a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Computational domain and boundary conditions</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/5481436/figures/5481436.fig.005b.svgz" name="5481436.fig.005b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Grid</td></tr></table>

<div>Computational domain model and grid. (a) Computational domain and boundary conditions. (b) Grid.</div>

International Journal of Aerospace Engineering

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Figure 5

Figure 5: Study on Size Distribution and Flow Characteristics of Condensed Products in Solid Rocket Motor 