Uncertainty analysis of global and local performance impact of inflow and geometric uncertainties using sparse grid-based non-intrusive polynomial chaos

Engineering

• Aerodynamics 100%
• Boundary Layer Separation 75%
• Mach Number 50%
• Compressor Blade 50%
• Engineering 25%
• Mathematical Model 25%
• Uncertainty Quantification 25%
• Edge Separation 25%
• Leading Edge 25%
• Suction Surface 25%
• Inlet Mach Number 25%
• Main Reason 25%
• Shape Design 25%
• Flow State 25%
• Operational Condition 25%
• Aerodynamic Analysis 25%
• Reference Flow 25%