Conceptual Aircraft Empennage Design Based on Multidisciplinary Design Optimization Approach

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/9288966/figures/9288966.fig.003a.svgz" name="9288966.fig.003a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Top view comparison</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/9288966/figures/9288966.fig.003b.svgz" name="9288966.fig.003b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Side view comparison</td></tr></table>

<div>Comparison of HTP, VTP, and wing optimized for minimal block fuel and MTOW.</div>

International Journal of Aerospace Engineering

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Figure 3

Figure 3: Conceptual Aircraft Empennage Design Based on Multidisciplinary Design Optimization Approach 