Experimental and numerical investigation of dual stage counter-rotating compressor

Engineering

• Rotors 100%
• Rotor Blade 50%
• Trailing Edge 50%
• Pressure Ratio 50%
• Incidence Angle 50%
• Flow Structure 50%
• Peak Efficiency 50%
• Blade Tip 50%
• Flow Separation 50%
• Energy Flow 50%
• Main Reason 50%
• Rotating Speed 50%