Design and analysis of a gas turbine blade by using FEM.

The main objective of the project is to improve the structural stability analysis of the gas turbine blade, in which the existing gas turbine blade is modeled in CATIA software and the modified model of the gas turbine blade is to make the geometrical change in the gas turbine base and the structural analysis, modal analysis and harmonic response analysis was done in ANSYS Workbench software. The INCONEL ALLOY 625, NICKEL ALLOY, NIMONIC ALLOY 80 A materials are compared for this structural analysis. [ABSTRACT FROM AUTHOR]