Design and Structural Thermal Analysis of Gas Turbine Rotor Blade with Radial Holes using Solidworks

Cooling of gas turbine blades are major attention to high temperature working conditions. Finally the blade with 9 holes has giving optimum performance for prescribed loading conditions with average temperature of 513.9 K, heat flux of 3.118 W m2 at the trailing edge and von misses stresses as 17.67 MPa. K Vidya Sagar | Dr. N. Mahesh Kumar | P. Siva Ram "Design and Structural Thermal Analysis of Gas Turbine Rotor Blade with Radial Holes using Solidworks" Published in International Journal of Trend in Scientific Research and Development (ijtsrd), ISSN: 2456-6470, Volume-3 | Issue-1 , December 2018, URL: https://www.ijtsrd.com/papers/ijtsrd19077.pdf Paper URL: http://www.ijtsrd.com/engineering/mechanical-engineering/19077/design-and-structural-thermal-analysis-of-gas-turbine-rotor-blade-with-radial-holes-using-solidworks/k-vidya-sagar