Constitutive modeling of solid propellant materials with evolving microstructural damage

Keyphrases

• Microstructural Damage 100%
• Constitutive Modeling 100%
• Solid Propellant 100%
• Void Growth 75%
• Composite Materials 50%
• Deformation Rate 50%
• Constitutive Response 50%
• Dewetting 25%
• Crack Tip 25%
• Oxidizer 25%
• Stress Relaxation 25%
• Constitutive Law 25%
• Fuel Particles 25%
• Mechanical Behavior 25%
• Law 25%
• Damage Evolution 25%
• Void nucleation 25%
• Decohesion 25%
• Constitutive Properties 25%
• Complex Loading Paths 25%
• Generic Forms 25%
• Back Stress 25%
• Homogenization Theory 25%
• Ammonium Perchlorate Particles 25%
• Compact Tension 25%
• Interface Void 25%
• Particle Phase 25%
• Particle Cracking 25%
• Extreme Temperature 25%
• High Elongation 25%
• Complex Microstructure 25%
• Tension Fracture 25%
• Fracture Specimens 25%
• Model Performance 25%
• Additive Decomposition 25%
• Uniaxial Tension Test 25%
• Polymer Interface 25%
• Individual Phases 25%
• Binder Phase 25%
• Viscous Deformation 25%
• Polymeric Binder 25%

Engineering

• Composite Material 100%
• Void Growth 100%
• Rate Deformation 100%
• Model Parameter 100%
• Binders 100%
• Constitutive Modeling 100%
• Crack Tip 50%
• Microstructure 50%
• Stress Relaxation 50%
• Decohesion 50%
• Damage Evolution 50%
• Individual Phase 50%
• Loading Path 50%
• Oxidizer 50%
• Additive Decomposition 50%

Material Science

• Constitutive Modeling 100%
• Solid Propellant 100%
• Composite Material 50%
• Void Growth 50%
• Nucleation 25%
• Crack Tip 25%
• Aluminum 25%
• Stress Relaxation 25%
• Polymer Particle 25%
• Tensile Testing 25%
• Damage Evolution 25%
• Mechanical Property 25%
• Homogenization 25%