Numerical investigation of unsteady shock wave motion in a transonic centrifugal compressor

Keyphrases

• Shock Waves 100%
• Wave Motion 100%
• Shock 100%
• Numerical Investigation 100%
• Unsteady Shock Wave 100%
• Transonic Centrifugal Compressor 100%
• Impeller 66%
• Boundary Layer 66%
• Vane 66%
• Transonic Compressor 66%
• Time-resolved 33%
• Three-dimensional (3D) 33%
• Performance Degradation 33%
• Efficiency Reduction 33%
• Turbocharger 33%
• High Pressure 33%
• Incidence Angle 33%
• Complex Interactions 33%
• Jet Structure 33%
• Stage Performance 33%
• Loss Generation 33%
• Pressure Wave 33%
• Tip Leakage Vortex 33%
• Diffuser 33%
• Diesel Engine 33%
• Inducer 33%
• Tip Leakage Flow 33%
• Mach number 33%
• Pressure Rise 33%
• Wake Structure 33%
• Diffuser Vane 33%
• Tip Clearance Flow 33%
• Unsteady Motion 33%
• Aerodynamic Loss 33%
• Static Pressure Drop 33%
• High Boost 33%
• Vortex Layer 33%
• Shock Motion 33%
• Shock Unsteadiness 33%
• Upstream Flow 33%
• Flow Unsteadiness 33%
• Flow Incidence 33%
• Vaned Diffuser 33%
• Automotive Engine 33%
• Boost Pressure 33%
• Reynolds-averaged Navier-Stokes 33%
• Marine Use 33%
• Stall Inception 33%
• Blade Row Interaction 33%
• Impeller-diffuser Interaction 33%
• Navier-Stokes Simulation 33%

Engineering

• Wave Motion 100%
• Diffusers 100%
• Centrifugal Compressor 100%
• Impeller 75%
• Shockwave 75%
• Boundary Layer 50%
• Pressure Rise 50%
• Performance Degradation 25%
• Vortex 25%
• Static Pressure 25%
• Supercharger 25%
• Diesel Engine 25%
• Leakage Flow 25%
• Incidence Angle 25%
• Relative Mach Number 25%
• Blade Row 25%