Robust optimization design of single-stage transonic axial compressor considering the manufacturing uncertainties

Keyphrases

• Single-stage Transonic Axial Compressor 100%
• Manufacturing Uncertainty 100%
• Robust Optimization Design 100%
• Tip Clearance 100%
• Total Pressure Ratio 66%
• Compressor Performance 66%
• Genetic Algorithm 33%
• Loss Model 33%
• Sensitivity Analysis 33%
• Probability Distribution 33%
• Mass Flow 33%
• Uncertainty Quantification 33%
• Effect on Performance 33%
• Navier-Stokes Solver 33%
• Reynolds-averaged Navier-Stokes 33%
• Rotor Efficiency 33%
• Non-intrusive Polynomial Chaos Expansion 33%
• Robust Design Optimization 33%
• Transonic Axial Compressor 33%
• Compressor Rotor 33%
• Rotor Design 33%
• Adiabatic Efficiency 33%
• Expansion Algorithm 33%
• Uncertainty Factors 33%

Engineering

• Compressor Performance 100%
• Axial Compressors 100%
• Pressure Ratio 100%
• Mean Value 50%
• Genetic Algorithm 50%
• Design Optimization 50%
• Reynolds-Averaged Navier-Stokes 50%
• Rotors 50%
• Uncertainty Quantification 50%
• Compressor Rotor 50%
• Robust Design 50%