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Simulation of progressive failure process in solid rocket propellants using a phase-field model

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Date of Publication:2024-11-16

Journal:Engineering Fracture Mechanics

Volume:312

ISSN No.:0013-7944

Key Words:Cracks; Digital elevation model; Fracture analysis; Fracture mechanics; HTPB; HTPB propellants; Interface crack; Interfaces (materials); Matrix crack; Phase field models; Progressive failure process; Rocket engines; Rockets; Solid rocket propellant; UMAT subroutine; Viscoelasticity; Visco-elastic material; Viscoelastic material

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