Finite Element Analysis of Adhesive Failure of Solid Composite Propellant Multi-material Structure for Underwater Intelligent Equipment

Abstract

This paper is a consecutive work based on the last paper “Finite element analysis of viscoelastic/damage behaviors of composite solid propellant for underwater intelligent equipment”. This paper studies adhesive failure behaviors of multi-material structure in underwater intelligent equipment, which includes the propellant layer/lining layer/adiabatic layer/aluminum layer. First, the hyperelastic mechanical properties for ethylene–propylene–diene monomer for adiabatic layer are predicted by using the Mooney–Rivlin constitutive model, where the material parameters are fitted by combining with theoretical and experimental load curves. Second, the adhesive failure between the propellant layer and the lining layer is predicted for the designed multiple material layers under shear loads by combining with the bilinear cohesive model, the constitutive models for the propellant and adiabatic layer materials. Finally, the adhesive failure mechanisms and the load responses are studied for the shear specimens.