Thermo-Structural Behaviour Prediction of the Nose Cap of a Hypersonic Vehicle Based on Multifield Coupling

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/3850283/figures/3850283.fig.008a.svgz" name="3850283.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Calorimetric perfect gas model</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2020/3850283/figures/3850283.fig.008b.svgz" name="3850283.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Chemical nonequilibrium gas model</td></tr></table>

<div>Comparison between the numerical and experimental results.</div>

International Journal of Aerospace Engineering

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Figure 8

Figure 8: Thermo-Structural Behaviour Prediction of the Nose Cap of a Hypersonic Vehicle Based on Multifield Coupling 