Surrogate models for performance prediction of axial compressors using through-flow approach

Engineering

• Empirical Model 100%
• Surrogate Model 100%
• Performance Prediction 100%
• Axial Compressors 100%
• Airfoil 60%
• Gaussians 40%
• Support Vector Machine 40%
• Two Dimensional 20%
• Pressure Ratio 20%
• Streamlines 20%
• Rotational Speed 20%
• Dimensional Analysis 20%
• Design Procedure 20%
• Pressure Loss 20%
• Internal Flow Field 20%
• Design Result 20%
• Dimensional Design 20%
• Learning Approach 20%
• Preliminary Design 20%
• Calculation Procedure 20%
• Final Design 20%
• Speed Line 20%