Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/1015674/figures/1015674.fig.007a.svgz" name="1015674.fig.007a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>The configuration of debris cloud</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2017/1015674/figures/1015674.fig.007b.svgz" name="1015674.fig.007b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Damage of the second layer of honeycomb sandwich panel</td></tr></table>

<div>Second layer of honeycomb sandwich panels (incidence angle is 30°).</div>

International Journal of Aerospace Engineering

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Figure 7

Figure 7: Numerical Simulation of Projectile Oblique Impact on Microspacecraft Structure 