Computational Procedure for the Life Assessment of Solid Rocket Motors
Author:
Affiliation:
1. Bogaziçi University, 34342 Istanbul, Turkey
Publisher
American Institute of Aeronautics and Astronautics (AIAA)
Subject
Space and Planetary Science,Aerospace Engineering
Link
https://arc.aiaa.org/doi/pdf/10.2514/1.46801
Reference18 articles.
1. On a fully three-dimensional finite-strain viscoelastic damage model: Formulation and computational aspects
2. Constitutive Modeling of High-Elongation Solid Propellants
3. Constitutive Equations for Solid Propellants
4. A nonlinear viscoelastic constitutive model of solidpropellant
5. Finite element formulation for modeling particle debonding in reinforced elastomers subjected to finite deformations
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