Nozzle design optimization for supersonic wind tunnel by using surrogate-assisted evolutionary algorithms

Engineering

• Nozzle 100%
• Optimization 66%
• Design 50%
• Algorithm 33%
• Measurement 33%
• Nozzle Exit 33%
• Design Optimization 33%
• Simulation 16%
• Experiments 16%
• Generates 16%
• High Precision 16%
• Airstream 16%
• Uniform Flow 16%
• Constraints 16%
• Viscosity 16%
• Horizontal Direction 16%
• Nozzle Design 16%
• Shape Design 16%
• Method of Characteristics 16%
• Shape Optimisation 16%
• Downstream Section 16%
• Flow Deflection 16%

Physics

• Optimization 66%
• Wind Tunnels 50%
• Boundary Layer 50%
• Supersonics 50%
• Correction 50%
• Algorithms 33%
• Mach Number 33%
• Design Optimization 33%
• Simulation 16%
• Regimes 16%
• Deviation 16%
• Adhesion 16%
• Contours 16%
• Computational Fluid Dynamics 16%
• Uniform Flow 16%
• Method of Characteristics 16%
• Flow Deflection 16%

Material Science

• Core Flow 50%