Turbomachinery Aerodynamics

Question 13: The critical zone for turbine blade cooling is

Stator exit station (near T.E)

Rotor exit station (near T.E.)

Stator entry station (near L.E.)            

Rotor entry station (near LE)
Prof. Bhaskar Roy, Prof. A M Pradeep, Department of Aerospace, IIT Bombay