Comparison of NPU and DLR design of axial-flow compressor rotor cascade

Engineering

• Axial-Flow Compressors 100%
• Compressor Rotor 100%
• Tunnel 50%
• Experimental Result 50%
• Design Optimization 50%
• Aerodynamic Design 50%
• Rotors 50%
• Two Dimensional 50%
• Operating Range 50%
• Inlet Mach Number 50%
• Aerodynamic Performance 50%
• Pressure Loss 50%
• Thickness Distribution 50%