An aerodynamic design and numerical investigation of transonic centrifugal compressor stage

Engineering

• Impeller 100%
• Computational Fluid Dynamics 100%
• Centrifugal Compressor Stage 100%
• Aerodynamic Design 100%
• One Dimensional 50%
• Flow Field 50%
• Pressure Ratio 50%
• Flow Structure 50%
• Leading Edge 50%
• Airfoil 50%
• Diffusers 50%
• Attack Angle 50%
• Flow Range 50%
• Relative Mach Number 50%
• Field Investigation 50%
• Span Increase 50%