Surrogate-based aerodynamic shape optimization of hypersonic flows considering transonic performance

Engineering

• Mach Number 100%
• Aerodynamic Shape Optimization 100%
• Hypersonic Flows 100%
• Surrogate Model 66%
• Transport Aircraft 66%
• Global Optimum 33%
• Computational Fluid Dynamics 33%
• Reynolds-Averaged Navier-Stokes 33%
• Airfoil 33%
• Objective Function 33%
• Computational Cost 33%
• Design Point 33%
• Aerodynamic Performance 33%
• Lift to Drag Ratio 33%
• Constraint Function 33%
• Flow Solver 33%
• Hypersonic Speed 33%
• Flow Regime 33%