The aim of the work is to define an automatic process and to combine specific Isight tools that allow engineers to match the thermal performance of an aero-engine turbine module with a thermal aero-engine FE Model. The thermal behaviors of a complex system are the result of strong interactions between the fluid-dynamics aspects and the heat balance within each component. All those phenomena are strictly connected and they are subjected to approximations coming from the input of the simulation model and from the interactions of different variables. These approximations are reflected on the final results.
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