Surrogate-based robust design optimization of airfoil using inexpensive Monte Carlo method

Engineering

• Aerodynamics 33%
• Airfoil 100%
• Angle-of-Attack 33%
• Candidate Design 33%
• Computational Fluid Dynamics 66%
• Design Optimization 100%
• Drag Coefficient 33%
• Flight Condition 33%
• Free-Stream Mach Number 33%
• Gaussians 33%
• Geometric Constraint 33%
• Good Agreement 33%
• Monte Carlo Approach 33%
• Objective Function 33%
• Optimization Technique 33%
• Output Response 33%
• Probability Density Function 100%
• Response Quantity 33%
• Robust Design 100%
• Statistical Moment 33%
• Surrogate Model 33%
• Uncertainty Quantification 33%