A Step-by-Step Equivalent Microprediction Method for the Mechanical Properties of Composite Solid Propellants considering Dewetting Damage

<div>Step-by-step equivalent microscopic finite element prediction model. (a) Containing small-sized particles. (b) Containing large-sized particles.</div>

International Journal of Aerospace Engineering

fig9

Figure 9

Figure 9: A Step-by-Step Equivalent Microprediction Method for the Mechanical Properties of Composite Solid Propellants considering Dewetting Damage 