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A Viscoelastic Constitutive Model of Propellant with Pressure Cure
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Outgoing claims: the papers this work cites, builds on, or argues with.
inferredcites →https://doi.org/10.1002/(sici)1097-0207(19970630)40:12<2267::aid-nme156>3.0.co;2-popenalex-snapshot
A THREE-DIMENSIONAL FINITE ELEMENT FORMULATION FOR THERMOVISCOELASTIC ORTHOTROPIC MEDIA
inferredcites →https://doi.org/10.1002/(sici)1097-4628(20000425)76:4<495::aid-app7>3.0.co;2-bopenalex-snapshot
Modeling the evolution of the dynamic mechanical properties of a commercial epoxy during cure after gelation
inferredcites →https://doi.org/10.1002/app.13416openalex-snapshot
Viscoelastic behavior of Cytec FM73 adhesive during cure
inferredcites →https://doi.org/10.1002/prep.201300120openalex-snapshot
Three‐dimensional Structural Analysis Approach for Aging Composite Solid Propellant Grains
inferredcites →https://doi.org/10.1002/prep.201900302openalex-snapshot
Thermodynamics and Kinetics of Curing Reaction Between Azide Binder ATP and Bispropargyl Succinate
inferredcites →https://doi.org/10.1002/prep.201900411openalex-snapshot
Simulation and Visual Tester Verification of Solid Propellant Slurry Vacuum Plate Casting
inferredcites →https://doi.org/10.1016/j.compositesa.2004.02.005openalex-snapshot
Prediction of shape distortions Part I. FE-implementation of a path dependent constitutive model
inferredcites →https://doi.org/10.1016/j.euromechsol.2016.10.002openalex-snapshot
A three-dimensional viscoelastic constitutive model of solid propellant considering viscoelastic Poisson's ratio and its implementation
inferredcites →https://doi.org/10.1080/10759419708945889openalex-snapshot
VISCOELASTIC ANALYSIS OF PROCESSING-INDUCED RESIDUAL STRESSES IN THICK COMPOSITE LAMINATES
inferredcites →https://doi.org/10.1106/yxea-5mh9-76j5-backopenalex-snapshot
A Plane Strain Model for Process-Induced Deformation of Laminated Composite Structures
inferredcites →https://doi.org/10.1177/002199839202600502openalex-snapshot
Process-Induced Stress and Deformation in Thick-Section Thermoset Composite Laminates
inferredcites →https://doi.org/10.2514/3.30412openalex-snapshot
Computing pressure cure viscoelastic effects in solid propellants.
inferredcites →https://doi.org/10.2514/3.6299openalex-snapshot
Stress waves in layered thermoelastic media generated by impulsive energy deposition
inferredcites →https://doi.org/10.2514/6.2010-6909openalex-snapshot
Pioneers in Propulsion-A History of CSD, Pratt & Whitney's Solid Rocket Company
What points at this work
Incoming claims: where this work appears in other papers’ reference lists and arguments.
inferred← citeshttps://doi.org/10.2139/ssrn.4771795openalex-extracted
Numerical and Experimental Study on the Curing Process of Nepe Solid Rocket Propellant Base on Thermo-Chemical-Mechanical Coupling
inferred← citeshttps://doi.org/10.1002/prep.70154openalex-snapshot
Pore Characteristics of NEPE Solid Propellant under Pressure Cure
inferred← citeshttps://doi.org/10.1007/s11340-025-01213-xopenalex-snapshot
In-Situ Monitor for Cure-Induced Deviatoric Stress in Propellant Charges of Solid Rocket Motors
inferred← citeshttps://doi.org/10.1007/s12289-025-01907-6openalex-snapshot
Pressure cure of solid propellant charge based on thermo-chemo-mechanical fully coupled viscoelastic model
inferred← citeshttps://doi.org/10.1007/s42401-024-00305-1openalex-snapshot
Prediction of burn rate of ammonium perchlorate–hydroxyl-terminated polybutadiene composite solid propellant using supervised regression machine learning algorithms
inferred← citeshttps://doi.org/10.1016/j.actaastro.2026.09.019openalex-snapshot
Stress evolution and process optimization in pressure-cured NEPE solid rocket motor grains: A thermo–chemo–viscoelastic analysis
inferred← citeshttps://doi.org/10.1016/j.csite.2024.105124openalex-snapshot
Numerical and experimental study on the curing process of NEPE solid rocket propellant considering multi-physical field effects
inferred← citeshttps://doi.org/10.1016/j.fpc.2026.02.005openalex-snapshot
Design of Temperature-Pressure Synergistic Curing Considering Pressure Effects on the Propellant Grain
inferred← citeshttps://doi.org/10.1016/j.matdes.2024.113261openalex-snapshot
Damage analysis of solid propellants with default defects based on macro-microscopic approach
inferred← citeshttps://doi.org/10.1088/1742-6596/3319/1/012003openalex-snapshot
The influence of mandrel constraint on the mechanical response of the grain during the curing and cooling process
inferred← citeshttps://doi.org/10.1155/2021/5026878openalex-snapshot
Analysis of Load Optimization in Solid Rocket Motor Propellant Grain with Pressure Cure
inferred← citeshttps://doi.org/10.1155/2023/8107966openalex-snapshot
Strain Prediction of Grain in Solid Rocket Motor under the Pressure Curing Molding Technology
inferred← citeshttps://doi.org/10.2139/ssrn.6591050openalex-snapshot
Investigation of Temperature–Pressure Coupling and Residual Stress Evolution in Pressurized Curing of NEPE Solid Propellants
inferred← citeshttps://doi.org/10.3390/polym15041019openalex-snapshot
Numerical Analysis of Curing Residual Stress and Strain in NEPE Propellant Grain
inferred← citeshttps://doi.org/10.4271/2026-99-1604openalex-snapshot
Experimental Study on The Parameters of the Viscoelastic-Plastic Constitutive Model of a Certain Solid Propellant
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