• AkashPahilwan
• Alisha Patel
• RuturajPatel

The turbine blades are responsible for extracting heat energy from high temperature, high-pressure gas. In the present paper, the base profile of the turbine rotor blade is selected depending on the application as a turbojet engine. The geometry of the first stage rotor blade is constructed and analyzed for fluid using the ANSYS software. Then the new rotor blade is designed with the modifications in the existing rotor blade and analyzed for flow for different parameters like incident angles and outlet angles. This process is carried out for a number of iterations and the optimal design of the turbine rotor blade is obtained which will give better sustainability in severe working conditions with the same flow pattern of the gaseous flow.

"Design and Analysis of Gas Turbine Rotor Blade", International Journal of Emerging Technologies and Innovative Research (www.jetir.org), ISSN:2349-5162, Vol.6, Issue 4, page no.900-904, April-2019, Available :http://www.jetir.org/papers/JETIRBB06171.pdf

"Design and Analysis of Gas Turbine Rotor Blade", International Journal of Emerging Technologies and Innovative Research (www.jetir.org | UGC and issn Approved), ISSN:2349-5162, Vol.6, Issue 4, page no. pp900-904, April-2019, Available at : http://www.jetir.org/papers/JETIRBB06171.pdf