Multi-objective aerodynamic design with user preference using truncated expected hypervolume improvement

Keyphrases

• User Preference 100%
• Expected Hypervolume Improvement 100%
• Aerodynamic Design 100%
• Multi-objective Bayesian Optimization 50%
• Multi-objective Optimization 16%
• Region of Interest 16%
• Design Process 16%
• General Trends 16%
• Pareto Front 16%
• Design Optimization 16%
• Process Optimization 16%
• Improvement Methods 16%
• Infill Criteria 16%
• Aerodynamics 16%
• Transonic Wing 16%
• Preliminary Design Stage 16%
• Coefficient Value 16%
• Control Characteristics 16%
• Absolute Value 16%
• Coarse Approximation 16%
• Transonic Airfoil 16%
• Pitching Moment 16%
• Fuel Burn 16%
• Kriging Model 16%
• Drag Coefficient 16%
• Inviscid 16%

Engineering

• Aerodynamic Design 100%
• Region of Interest 33%
• Design Process 33%
• Design Optimization 33%
• Airfoil 33%
• Pareto Front 33%
• Objective Function 33%
• Multiobjective Optimization 33%
• Preliminary Design Phase 33%
• Pitching Moment 33%
• Kriging Model 33%
• Drag Coefficient 33%
• Absolute Value 33%