Расчет нестационарного температурного состояния деталей двигателя по граничным условиям III рода, полученным из двумерного теплогидравлического расчета

Abstract

There is a calculation method, which is allowing to obtain an nsteady-state temperature field for a gas-turbine engine’s parts using third kind boundary conditions obtained from a two-dimensional thermohydraulic model. The main benefit of this method is probability to save time because the direct 3D calculations of conjugate heat transfer no more needed. In current article details of algorithm, method and its validation are represented.