Surrogate-based robust airfoil design under aleatory operating-conditions and geometric uncertainties

Engineering

• Airfoil 100%
• Robust Design 100%
• Integral Method 100%
• Mach Number 66%
• Surrogate Model 66%
• Computational Fluid Dynamics 66%
• Drag Coefficient 66%
• Design Optimization 33%
• Optimization Method 33%
• Aerodynamic Design 33%
• Angle-of-Attack 33%
• Objective Function 33%
• Flight Condition 33%
• Aerodynamic Characteristic 33%
• Sample Point 33%
• Probability Distribution Function 33%
• Pitching Moment 33%
• Constrained Optimization Problem 33%
• Deterministic Design 33%
• Design of Experiment Method 33%