Experimental investigation on the performance of compressor cascade using blended-blade-end-wall contouring technology

Engineering

• Airfoil 50%
• Control Flow 50%
• Dimensional Flow Separation 50%
• Experimental Investigation 100%
• Experimental Result 50%
• Flow Separation 50%
• Incidence Angle 50%
• Main Reason 50%
• Numerical Methods 50%
• Performance Improvement 50%
• Pressure Loss 50%
• Suction Surface 100%
• Vortex 50%