Use Fuzzy Neural Network to Model Gas Turbine Cooled Blades

In this paper, the mathematical models and high effective combination numerical methods for calculating of stationary and dynamic temperature field of a profile part of a blade with convective cooling are put forward. The theoretical substantiation of these methods is proved by appropriate theorems. For it, converging integral processes have been developed and the estimations of errors in the terms of Karnel continuity modules have been received. Boundary conditions of heat exchange are determined by the solution of the corresponding integral equations and empirical relationships. The reliability of designed methods is proved by calculation and experimental investigation heat and hydraulic characteristics of the gas turbine