Numerical investigation on aerodynamic characteristics of exhaust passage with consideration of multi-factor components in a supercritical steam turbine

Engineering

• Aerodynamic Characteristic 100%
• Supercritical Steam 100%
• Steam Turbine 100%
• Pressure Recovery Coefficient 66%
• Static Pressure 66%
• Exhaust Hood 66%
• Enthalpy Drop 66%
• Specific Enthalpy 66%
• Flow Characteristic 33%
• Aerodynamic Performance 33%
• Pressure Loss 33%
• Phase Model 33%
• Condenser 33%
• Last-Stage Blade 33%
• Local Loss 33%
• Pressure Steam 33%