Investigation on the shock control using grooved surface in a linear turbine nozzle

Engineering

• Computer Simulation 100%
• Engine Performance 33%
• Exit Plane 33%
• Expansion Ratio 33%
• Fatigue Failure 33%
• Flow Variable 33%
• High Cycle Fatigue 33%
• Impeller 66%
• Leakage Flow 33%
• Nozzle Vane 33%
• Point Operation 33%
• Radial Flow 33%
• Rotors 33%
• Schlieren 66%
• Smooth Surface 66%
• Static Pressure 33%
• Trailing Edge 33%
• Turbocharger 33%