THERMAL AND STRUCTURAL ANALYSIS OF T6, HAYNES 188 AND X-40 GAS TURBINE BLADE AT VARIOUS OPERATING TEMPERATURES
Gas turbine blades operate under extreme thermal and mechanical loads, requiring efficient cooling strategies and materials with high-temperature resistance. This study presents a comparative thermal and structural analysis of blades made from Ti-T6, Haynes 188, and X-40 using finite element analysis (FEA). Blade model...