Influence of Solidity on Aerodynamic Performance of Axial Supersonic Through-Flow Fan Cascades

Engineering

• Aerodynamic Performance 100%
• Boundary Layer 50%
• Computer Simulation 50%
• Flow Structure 50%
• Fluid Viscosity 50%
• Induced Separation 50%
• Inlet Mach Number 50%
• Layer Interaction 50%
• Leading Edge 50%
• Pressure Side 50%
• Reflected Shock 50%
• Suction Surface 100%
• Trailing Edge 50%