Study of the Mechanical Properties of a CMDB Propellant Over a Wide Range of Strain Rates Using a Group Interaction Model

<table class="figure-group"><tr class="fig-image" id="a"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/7099199/figures/7099199.fig.001a.svgz" name="7099199.fig.001a" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(a) </b>Specimen for the low and medium strain rate uniaxial compression tests</td></tr><tr class="fig-image" id="b"><td><object data="https://static-preview.hindawi.com/articles/ijae/volume-2022/7099199/figures/7099199.fig.001b.svgz" name="7099199.fig.001b" type="image/svg+xml"></object></td></tr><tr class="fig-caption"><td><b>(b) </b>Specimen for the high strain rate uniaxial compression tests</td></tr></table>

<div>Specimen for the uniaxial compression test.</div>

International Journal of Aerospace Engineering

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Figure 1

Figure 1: Study of the Mechanical Properties of a CMDB Propellant Over a Wide Range of Strain Rates Using a Group Interaction Model 