Impacts of Tandem Configurations on the Aerodynamic Performance of an Axial Supersonic Through-Flow Fan Cascade

Engineering

• Aerodynamic Performance 100%
• Airfoil 50%
• Chord Length 50%
• Computer Simulation 50%
• Design Tandem 50%
• Flow Structure 50%
• Load Distribution 50%
• Pressure Loss 50%
• Pressure Loss Coefficient 50%
• System Structure 50%
• Throughflow 100%