Structural integrity analysis for the canular solid propellant grains subjected to temperature loading

Engineering

• Structural Integrity 100%
• Expansion Coefficient 66%
• Low-Temperature 33%
• Transients 33%
• Temperature Field 33%
• Strain 33%
• Large Deformation 33%
• Finite Element Modeling 33%
• Thermal Stress 33%
• Constitutive Equation 33%
• Equivalent Strain 33%
• Equivalent Stress 33%
• Lagrangian Method 33%
• Temperature Time 33%
• Strain Response 33%