Study on the Interaction of Clearance Flow and Shock Wave in a Turbine Nozzle

Engineering

• Impeller 100%
• Nozzle Vane 100%
• Computer Simulation 50%
• Rotors 50%
• Flow Structure 50%
• Operating Point 50%
• Engine Operating Point 50%
• Main Flow 50%
• Static Pressure 50%
• Turbocharger 50%
• Transient Analysis 50%
• High Cycle Fatigue 50%
• Turbine Efficiency 50%
• Schlieren 50%
• Expansion Ratio 50%
• Interaction Region 50%
• Development Process 50%
• Leakage Flow 50%
• Flow Visualization 50%
• Interaction Behavior 50%
• Radial Flow 50%
• Flow Variable 50%