Calculation of intake-fan-bypass interaction with a fan similarity model

Engineering

• Similarities 100%
• Fan Blade 100%
• Boundary Condition 100%
• Duct 50%
• Time Domain 50%
• Frequency Domain 50%
• Spatial Resolution 50%
• Airfoil 50%
• Axisymmetric 50%
• Guide Vane 50%
• Design Stage 50%
• Aero-Engines 50%
• Propulsive Efficiency 50%
• Transonic Flow 50%
• Coupled System 50%
• Specific Fuel Consumption 50%
• Bypass Ratio 50%
• Fan Inlet 50%
• Blade Passing Frequency 50%
• Flight Condition 50%
• Flow Distribution 50%