Modeling of Spray Combustion with a Steady Laminar Flamelet Model in an Aeroengine Combustion Chamber Based on OpenFOAM

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7329564/figures/7329564.fig.0015a.svgz" name="7329564.fig.0015a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>The mass fraction of C<sub>12</sub>H<sub>23</sub></td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7329564/figures/7329564.fig.0015b.svgz" name="7329564.fig.0015b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>The mass fraction of CO<sub>2</sub></td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7329564/figures/7329564.fig.0015c.svgz" name="7329564.fig.0015c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>The mass fraction of H<sub>2</sub>O</td></tr><tr class="fig-image" id="d"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/7329564/figures/7329564.fig.0015d.svgz" name="7329564.fig.0015d" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(d) </b>The mass fraction of OH</td></tr></table>

<div>The mass fraction of species contours for the center plane.</div>

International Journal of Aerospace Engineering

fig15

Figure 15

Figure 15: Modeling of Spray Combustion with a Steady Laminar Flamelet Model in an Aeroengine Combustion Chamber Based on OpenFOAM 