Design of a rear-stage subsonic axial compressor with casing treatments

Keyphrases

• Aerodynamic Design 33%
• Airfoil 33%
• ANSYS CFX 33%
• Axial Compressor 100%
• Axial Slot Casing Treatment 33%
• Blade Count 33%
• Blade Design 66%
• Blade Loading 33%
• Casing Treatment 100%
• Controlled Diffusion 33%
• Design of Experiments 66%
• Double-leakage 33%
• Efficiency Benefit 33%
• Efficiency Increase 33%
• Efficiency Penalty 33%
• Flow Solver 33%
• Friction Loss 33%
• Friction Reduction 66%
• Gas Path 33%
• Geometric Properties 33%
• High Pressure 33%
• Inviscid 33%
• Large Rotor 33%
• Local Stage 33%
• Low Aspect Ratio 33%
• NavierStokes 33%
• Off-design Performance 33%
• Reynolds-averaged 33%
• Rotor 100%
• Rotor Blade 33%
• Rotor Tip 33%
• Secondary Flow Loss 33%
• Simulation ANSYS 33%
• Stage Design 33%
• Stall 33%
• Stall Margin 66%
• Stator 100%
• Sweeping 33%
• Tip Gap 33%
• Tip Vortex 33%

Engineering

• Aerodynamic Design 25%
• Airfoil 25%
• Aspect Ratio 25%
• Axial Compressors 100%
• Blades Design 50%
• Casing Treatment 100%
• Design of Experiments 50%
• Design Stage 25%
• Flow Loss 25%
• Flow Solver 25%
• Friction Loss 25%
• Rotor Blade 25%
• Rotors 100%
• Secondary Flow 25%
• Vortex 25%