Design and Thermal analysis by using Finite Element Method for Gas Turbine Rotor Blade
- A.Gowrishankar
- S.Ranganathan
Thermal Analysis, Modal, Finite Element Analysis, Gas Turbine.
Withstanding of gas turbine blades for the elongations is a major consideration in their design because they are subjected to high tangential, axial, centrifugal forces during their working conditions. The first stage rotor blade of a two-stage gas turbine has been analyzed for structural, thermal using ANSYS 12 which is powerful Finite Element Software. In the process of getting the thermal stresses, the temperature distribution in the rotor blade has been evaluated using this software. This project specifies how the program makes effective use of the ANSYS pre-processor to analyse the complex turbine blade geometries and apply boundary conditions to examine steady state thermal & structural performance of the blade for N 155, Hastealloy x & Inconel 625 materials.
A.Gowrishankar, S.Ranganathan. "Design and Thermal analysis by using Finite Element Method for Gas Turbine Rotor Blade".INTERNATIONAL JOURNAL OF ENGINEERING DEVELOPMENT AND RESEARCH ISSN:2321-9939, Vol.3, Issue 2, pp.166-169, URL :https://rjwave.org/ijedr/papers/IJEDR1502030.pdf
Volume 3 Issue 2
Pages. 166-169
