Experimental and numerical investigation on the aerodynamic performance of a compressor cascade using blended blade and end wall

Engineering

• Numerical Study 100%
• Aerodynamic Performance 100%
• Flow Field 66%
• Experimental Result 33%
• Limitations 33%
• Internals 33%
• Computational Fluid Dynamics 33%
• Performance Improvement 33%
• Suction Side 33%
• Flow Loss 33%
• Design Point 33%
• Suction Surface 33%
• Incidence Angle 33%
• Pressure Loss Coefficient 33%
• Low Wind Speed 33%