Mechanism analysis of stability improvement with tip injection in a transonic axial-flow compressor rotor

Engineering

• Rotors 100%
• Vortex 100%
• Axial-Flow Compressors 100%
• Compressor Rotor 100%
• Predicted Result 50%
• Multichannel 50%
• Incidence Angle 50%
• NASA 50%
• Blade Tip 50%
• Flow Passage 50%
• Energy Region 50%
• Electric Inductors 50%
• Reinjection 50%
• Diffusion Factor 50%
• Annulus Flow 50%