Numerical Simulation of Temperature Distribution in the Gas Turbine Blade

This paper concentrates on temperature distribution in the gas turbine blade equipped by cooling holes system transient heat transfer. The present study requires specification of internal and external boundary conditions. calculations had been done using both Crank-Nicolson algorithm, explicit implicit methods, which different transfer coefficients surfaces were applied. value has a direct crucial impact final result. coefficient working surface pipes was 1600 W/(m2K). It found that there no significant differences comparison results from method Ansys analysis, algorithm Matlab. simulation is based Finite Element Method, uses Crank Nicolson algorithm.