Call For Paper Volume:7 Issue:9 Sep'2020 |

THERMAL ANALYSIS OF A GAS TURBINE BLADE

Publication Date : 22/08/2016


DOI : 10.21884/IJMTER.2016.3011.MYPSY

Author(s) :

N VINAY KUMAR , P.RAJU , P.SRINIVASULU.


Volume/Issue :
Volume 3
,
Issue 8
(08 - 2016)



Abstract :

In this thesis a turbine blade is designed and modeled in Pro/Engineer software. The turbine blades are cooled using film cooling. The turbine blade with film cooling for no holes, 3 holes, 7 holes, 13 holes is modeled. CFD, Thermal analysis is done to determine the heat transfer rates, heat transfer coefficients of the blade. The present used material for blade is chromium steel. In this thesis, it is replaced with Nickel alloys. The better material for blade is analyzed. Key words: Turbine blade, Heat transfer rate, Heat transfer coefficient, Chromium steel, Nickel alloy


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THERMAL ANALYSIS OF A GAS TURBINE BLADE

August 16, 2016