Mod-01 Lec-22 Axial Flow Turbines: Blade and Axial Flow Passages, Exit Flow Matching with Nozzle
Channel: nptelhrd
Date: 2015-03-12

Turbomachinery Aerodynamics by Prof. Bhaskar Roy,Prof. A M Pradeep, Department of Aerospace Engineering,  IIT Bombay. For more details on NPTEL visit http://nptel.ac.in