Mod-01 Lec-22 Axial Flow Turbines: Blade and Axial Flow Passages, Exit Flow Matching with Nozzle
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06 Jul 2019
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Maths & Sciences / Physique, chimie
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
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