Surrogate-based aerodynamic shape optimization of a wing-body transport aircraft configuration

Engineering

• Aerodynamic Shape Optimization 100%
• Surrogate Model 100%
• Transport Aircraft 100%
• Computational Fluid Dynamics 50%
• Reynolds-Averaged Navier-Stokes 50%
• Computational Cost 50%
• Local Optimum 50%
• Drag Coefficient 50%
• Final Result 50%
• Flow Solver 50%
• Freeform Deformation 50%
• Design Space 50%
• Sample Point 50%
• Computational Grid 50%
• Aerodynamic Coefficient 50%
• Complex Aircraft 50%
• Civil Transport Aircraft 50%