CFD Analysis of Film Cooling in Gas Tusrbine Blade

Kumar, Sandeep (2015) CFD Analysis of Film Cooling in Gas Tusrbine Blade. BTech thesis.



This project is about an exhaustive investigation of film cooling of gas turbine blade using ANSYS WORKBENCH version 15.0. Film cooling has its application in gas turbine blade. Film cooling and turbulated internal cooling is used by Gas turbines to guard the outer surfaces of blades from hot gases. The study focuses on film cooling effect for modern turbine blades. The adiabatic film effectiveness and heat transfer coefficient are found out experimentally over a flat plate downstream of line of incline. The study also involves investigation of various advanced hole geometries that would result in effective film cooling effect over turbine airfoil and flat surfaces. The systems of the jets are understood by film cooling predictions. FLUENT computer code was used to run the simulation of turbulent flows in film cooling. This simulation used RSM (Reynolds’ Stress Transport Model).

Item Type:Thesis (BTech)
Uncontrolled Keywords:CFD, Film Cooling, Gas Turbine Blade, Fluent
Subjects:Engineering and Technology > Mechanical Engineering > Computational Fluid Dynamics
Divisions: Engineering and Technology > Department of Mechanical Engineering
ID Code:7577
Deposited By:Mr. Sanat Kumar Behera
Deposited On:18 Sep 2016 21:00
Last Modified:18 Sep 2016 21:00
Supervisor(s):Satapathy, A K

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