Evaluation and analysis of evaporation cooling on thermodynamic and pressure characteristics of intake air in a precooled turbine engine

Engineering

• Turbine 100%
• High Mach Number 66%
• Inlet Air 66%
• Water Injection 66%
• Mach Number 33%
• Pressure Drop 33%
• Flow Distribution 33%
• Drag Reduction 33%
• Flow Velocity 33%
• Flow Rate 33%
• Flow Loss 33%
• Temperature Drop 33%
• Pressure Loss 33%
• Multiphase Flow 33%
• Resistance Characteristic 33%
• Pressure Flow 33%
• Cooling Section 33%
• Field Uniformity 33%
• Thermodynamic Process 33%