Influences of geometric parameters on serpentine nozzles for turbofan

Engineering

• Geometric Parameter 100%
• Flow Distribution 66%
• Aerodynamic Performance 66%
• Vortex 33%
• Local Minimum 33%
• Numerical Prediction 33%
• Aero-Engines 33%
• Numerical Method 33%
• Flow Characteristic 33%
• Shear Layer 33%
• Relative Error 33%
• Flow Visualization 33%
• Internal Flow 33%
• Flow Separation 33%
• Velocity Fluctuation 33%
• Scale Model 33%
• Discharge Coefficient 33%
• Stress Region 33%
• Schlieren 33%
• Mixers (Machinery) 33%
• Limiting Streamlines 33%
• High Velocity Region 33%
• Exhaust Systems (Engine) 33%