Coupling optimization design for aspirated compressor airfoil and aspirated scheme

Engineering

• Design Optimization 100%
• Airfoil 100%
• Design Condition 75%
• Optimised Design 50%
• Tunnel 25%
• Design Method 25%
• Boundary Layer 25%
• Layer Flow 25%
• Inlet Mach Number 25%
• Boundary Layer Separation 25%
• Design Analysis 25%
• Scheme Design 25%
• Pressure Loss 25%
• Leading Edge Radius 25%
• Load Distribution 25%
• Boundary Layer Transition 25%
• Control Boundary 25%
• Friction Loss 25%
• Airflow Rate 25%