Effective Mechanical Property Estimation of Composite Solid Propellants Based on VCFEM

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/2050876/figures/2050876.fig.008a.svgz" name="2050876.fig.008a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td>(a) Effective Young’s modulus versus Vf and VAP/VAl</td></tr><tr class="fig-image" id="b"><td><object data="https://static.hindawi.com/articles/ijae/volume-2018/2050876/figures/2050876.fig.008b.svgz" name="2050876.fig.008b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td>(b) Effective Poisson’s ratio versus Vf and VAP/VAl</td></tr></table>

<div>Effective properties of solid propellants versus Vf and VAP/VAl.</div>

International Journal of Aerospace Engineering

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Figure 8

Figure 8: Effective Mechanical Property Estimation of Composite Solid Propellants Based on VCFEM 