Study of Cooldown Thermal Loading Effect on the Bore Deformation of Viscoelastic Solid Propellant Grain
Author:
Affiliation:
1. Beihang University
Publisher
American Institute of Aeronautics and Astronautics
Link
https://arc.aiaa.org/doi/pdf/10.2514/6.2017-4692
Reference25 articles.
1. R. Marimuthu, B.N. Rao, "Development of efficient finite elements for structural integrity analysis of solid rocket motor propellant grains", Int. J. Press. Vessels Piping 111-112,2013, pp.131-145.
2. Constitutive Modeling of High-Elongation Solid Propellants
3. On a fully three-dimensional finite-strain viscoelastic damage model: Formulation and computational aspects
4. A three-dimensional nonlinear viscoelastic constitutive model of solid propellant
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