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The Effect of Cooling-Air Flow Conditions on the Thermal State of High-Pressure Nozzle Blade

Developing technique utilized for cooling turbine blades plays an important role in designing as well as manufacturing Gas Turbine Engine (GTE). This may enhance the GTE's lifetime and decrease its fuel consumption. The paper numerically examines the effect of cooling-air mass flow rate and other flow conditions including temperature and pressure on the thermal state of high-pressure nozzle blade of the DR 76 gas turbine engine.