An Improved Nonlinear Aerodynamic Derivative Model of Aircraft at High Angles of Attack

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/5815167/figures/5815167.fig.006a.svgz" name="5815167.fig.006a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Lift coefficient</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2021/5815167/figures/5815167.fig.006b.svgz" name="5815167.fig.006b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Pitch moment coefficient</td></tr></table>

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International Journal of Aerospace Engineering

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Figure 6

Figure 6: An Improved Nonlinear Aerodynamic Derivative Model of Aircraft at High Angles of Attack 