Uncertainty quantification and global sensitivity analysis for hypersonic aerothermoelastic analysis

Engineering

• Temperature Distribution 100%
• Uncertainty Quantification 100%
• Control Surface 50%
• Computational Fluid Dynamics 33%
• Integration Method 33%
• Numerical Integration 33%
• Aerodynamics 16%
• Parameter Uncertainty 16%
• Thermal Stress 16%
• Resonant Frequency 16%
• Aeroelasticity 16%
• Navier-Stokes Equation 16%
• Coefficient of Variation 16%
• Hypersonic Flows 16%
• Parameterized Model 16%
• Stability Boundary 16%
• Aerothermodynamics 16%

Material Science

• Aeroelasticity 33%

Physics

• Aerothermoelasticity 16%