Modeling of Ice Accretion over Aircraft Wings Using a Compressible OpenFOAM Solver

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4864927/figures/4864927.fig.0011a.svgz" name="4864927.fig.0011a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Section A</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4864927/figures/4864927.fig.0011b.svgz" name="4864927.fig.0011b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Section B</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2019/4864927/figures/4864927.fig.0011c.svgz" name="4864927.fig.0011c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Section C</td></tr></table>

<div>Pressure coefficient at three ONERA M6 wing sections.</div>

International Journal of Aerospace Engineering

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Figure 11

Figure 11: Modeling of Ice Accretion over Aircraft Wings Using a Compressible OpenFOAM Solver 