• korrapati lakshmi prasanna
• A.Surendra

Gas turbine has become main functional part of many applications. Blades are considered as the heart of turbine and all other member exist for the sake of the blades. The turbine blade gets effected because the gas coming out from combustion chamber at a high temperature and high velocity. So the point of this undertaking is to examine a gas turbine blade with distinctive kind of alloys for high strength against high temperature effect and different hassles effect. In this task three distinctive and respectable Ni based, high temperature withstanding alloys designed in this field. Withstanding of gas turbine blades for the prolongations is a noteworthy thought in their configuration of the way that they are subjected to high tangential loads during their working conditions. A few systems have been proposed for the better improvement of the mechanical properties of blades to withstand these extreme conditions. This project explains designing and analysis of Gas turbine blade, Catia V5 R20 software is used to design the blade with the help of 2D and 3D commands and the analysis of blade is done in ANSYS 15.07 software by meshing the blade and applying the boundary conditions.

"Design And Analysis Of Gas Turbine Rotor Blade With Variation Of Holes By Using FEA Approach ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 6, page no.640-646, June 2019, Available :http://www.jetir.org/papers/JETIR1907J82.pdf

"Design And Analysis Of Gas Turbine Rotor Blade With Variation Of Holes By Using FEA Approach ", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 6, page no. pp640-646, June 2019, Available at : http://www.jetir.org/papers/JETIR1907J82.pdf