Turbomachinery Aerodynamics

Question 18: In axial compressor rotor airfoil shape is harnessed in the following manner


L.E. portion creates suction, rest of the airfoil diffuses

Creates a convergent-divergent bladed passage                       

Transfers energy to air with minimum loss                    

All the above together

Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay