Blade Meridional Profile Optimization for Novel High-Pressure Ratio Centrifugal Compressor Design Using Numerical Simulations

Keyphrases

• Numerical Simulation 100%
• Profile Optimization 100%
• Meridional Profile 100%
• High Pressure Ratio Centrifugal Compressor 100%
• Centrifugal Compressor Performance 100%
• Stall 66%
• Meridional Contours 66%
• Centrifugal Compressor 66%
• Operating Range 33%
• Performance Parameters 33%
• Aerospace 33%
• Effect on Performance 33%
• Turbulence 33%
• Novel Design 33%
• Pressure Ratio 33%
• Turbocharger 33%
• Numerical Investigation 33%
• Design Procedure 33%
• Structured Mesh 33%
• Design Condition 33%
• Mass Flow Rate 33%
• ANSYS CFX 33%
• High Rotational Speed 33%
• Isentropic Efficiency 33%
• Pressure Efficiency 33%
• 3D numerical Simulation 33%
• Reynolds-averaged Navier-Stokes 33%
• High Pressure Ratio 33%
• Transonic 33%
• SRV2 33%
• Stall Margin 33%
• Blade Thickness 33%
• Centrifugal Compressor Impeller 33%
• Total Pressure Ratio 33%

Engineering

• Centrifugal Compressor 100%
• High Pressure Ratio Centrifugal Compressor 100%
• Pressure Ratio 66%
• Electric Inductors 66%
• Operating Range 33%
• Performance Parameter 33%
• Impeller 33%
• Turbocharger 33%
• Design Procedure 33%
• Structured Mesh 33%
• Design Condition 33%
• Mass Flowrate 33%
• Rotational Speed 33%
• Isentropic Efficiency 33%
• High Pressure Ratio 33%
• Reynolds-Averaged Navier-Stokes 33%
• Blade Thickness 33%