A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/897213/figures/897213.fig.005a.svgz" name="897213.fig.005a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Test</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2015/897213/figures/897213.fig.005b.svgz" name="897213.fig.005b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Simulation</td></tr></table>

<div>Overpressure versus time curves of pressure sensors in test (a) and simulation (b) with similar axes scale.</div>

International Journal of Aerospace Engineering

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Figure 5

Figure 5: A Numerical Method for Blast Shock Wave Analysis of Missile Launch from Aircraft 