Multidisciplinary Design Optimization of Reentry-Powered Hypersonic Vehicles Based on Surrogate Model

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2024/5557153/figures/5557153.fig.003a.svgz" name="5557153.fig.003a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Schematic of vehicle design parameters</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2024/5557153/figures/5557153.fig.003b.svgz" name="5557153.fig.003b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Schematic diagram of vehicle body shape lines and contour curves</td></tr><tr class="fig-image" id="c"><td><object data="https://static.hindawi.com/articles/ijae/volume-2024/5557153/figures/5557153.fig.003c.svgz" name="5557153.fig.003c" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(c) </b>Generated vehicle configurations</td></tr></table>

<div>Parameterized configuration of the vehicle.</div>

International Journal of Aerospace Engineering

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Figure 3

Figure 3: Multidisciplinary Design Optimization of Reentry-Powered Hypersonic Vehicles Based on Surrogate Model 